Launch Vehicles

Abyom-Spacetech enables frequent, low-cost deployment of satellites and orbital assets, supports defense and meteorological missions, facilitates microgravity experiments, and provides rocket engine t

Abyom Spacetech

Medium Reusable Launch Vehicle (MRLV)

Heavy-lift orbital launch vehicle — 15 t to LEO (reusable) or 2 t to GTO — 75 m tall, 9× AbyoKalam-950 LOX/LNG engines for telecom, defense, and cargo missions.

Height	75 m
Diameter	4.8 m
Payload (reusable) to LEO	15 t
Payload (reusable) to SSO	9 t
Payload (reusable) to GTO	2 t

price on request

Abyom Spacetech

Reusable Sounding Rocket

Two-stage reusable sounding rocket delivering 200 kg to LEO — 5× AbyoKalam-35 LOX/LNG engines, 16 m booster, designed for atmospheric research and microgravity experiments.

Payload capacity	200 kg to LEO
Booster stage	16 m height × 1.8 m diameter
Payload stage	16 m height × 2 m diameter
Propellant	LOX/LNG
Engine model	AbyoKalam-35

price on request

Abyom Spacetech

Small Reusable Launch Vehicle (SRLV)

Orbital small launch vehicle with 2.6 t to LEO (reusable) or 7 t (expendable) — 9× AbyoKalam-350 LOX/LNG engines, 55 m tall, targeting commercial small satellite operators.

Height	55 m
Diameter	3 m
Payload (reusable) to LEO	2.6 t
Payload (reusable) to SSO	1 t
Payload (expendable) to LEO	7 t

price on request

US autonomous launch company developing Ravn X, an unmanned, runway-launched, reusable autonomous launch vehicle (AuLV) for rapid small-satellite deployment to low Earth orbit.

Aevum

Ravn X Autonomous Launch System

Aevum's autonomous drone carrier aircraft (Ravn X) that air-launches a two-stage orbital rocket — targeting up to 100 kg to SSO with fully autonomous end-to-end operations.

Carrier Vehicle	Ravn X — autonomous jet-powered UAS
Launch Method	Air-launch from Ravn X aircraft
Payload to SSO	Up to 100 kg
Key Feature	Fully autonomous (no pilots, no ground controllers)
Military Applications	Tactically Responsive Launch (AFRL, US Space Force contracts)

price on request

Agnikul Cosmos designs, manufactures, and launches orbital-class vehicles using 3D-printed engines and a mobile launchpad, providing dedicated and flexible access to space.

Agnikul Cosmos

Agnibaan

Agnibaan is Agnikul Cosmos' fully indigenous, customizable small-satellite launch vehicle powered by the world's first single-piece, fully 3D-printed semi-cryogenic engine, Agnilet

Height	~18 m
Diameter	1.3 m
Liftoff mass	~14,000 kg
Stages	2, configurable, with optional 'baby stage' inside payload fairing
Engine	Agnilet - semi-cryogenic, LOX/kerosene, electric-pump-fed, single-piece fully 3D-printed,

price on request

Agnikul Cosmos

Agnibaan SOrTeD

Agnikul Cosmos's single-stage suborbital demonstrator that became the world's first launch of a single-piece 3D-printed rocket engine.

Type	Suborbital Technology Demonstrator
Engine	Agnilet (single-piece 3D-printed, LOX/Kerosene)
Engine Thrust	~6 kN
Flight Date	May 30, 2024
Achievement	World's first flight of a single-piece 3D-printed engine

price on request

Aphelion Orbitals is a New Jersey-based launch vehicle company developing the Helios nanosatellite launch system for regular, scheduled orbital access at low cost.

Aphelion Orbitals

Helios and Trailblazer Launch Vehicles

Helios and Trailblazer are responsive, dedicated launch and suborbital access solutions designed for high cadence and mass production, providing regular, scheduled orbital access f

Payload to SSO	20 kg
Target Orbit	Sun-Synchronous Orbit (SSO)
Launch Cadence	Regular scheduled launches
Configuration	Dedicated nanosatellite launcher

price on request

ArianeGroup designs and manufactures space transport systems, including launchers and related technologies, for institutional, commercial, and industrial customers in civil and military sectors.

arianegroup

Ariane 6 Launch Vehicle

European heavy-lift launch vehicle — A62 (two boosters, 10.3 t to GTO) and A64 (four boosters, 21.6 t to GTO), Vulcain 2.1 core + Vinci upper stage, first flight July 2024.

Configurations	A62 (2 boosters), A64 (4 boosters)
GTO payload (A62)	10.3 t
GTO payload (A64)	21.6 t
Core engine	Vulcain 2.1 (cryogenic, 136 kN vacuum)
Upper stage engine	Vinci (restartable, 180 kN vacuum)

price on requestdatasheet

European launch services operator — Ariane 6, Vega C — heavy GTO/GEO and SSO rideshare.

Arianespace

Ariane 6

Europe's next-generation heavy-lift expendable launch vehicle, available in two- and four-booster configurations for a range of orbits.

Ariane 62 payload to GTO	~3,500 kg
Ariane 64 payload to GTO	~5,000 kg
Ariane 62 payload to LEO	~10,300 kg
Ariane 64 payload to LEO	~21,600 kg
Upper stage engine	Vinci (restartable, LOX / LH2)

price on requestdatasheet

Arianespace

Vega

Europe's retired small satellite dedicated launcher that flew 22 missions from 2012 to 2024 with a 91% success rate.

Payload to SSO (700 km)	~1,430 kg
Payload to Polar Orbit (400 km)	~1,450 kg
Stage 1 (P80FW) Thrust	2,261 kN
Stage 2 (Zefiro-23) Thrust	871 kN
Stage 3 (Zefiro-9) Thrust	260 kN

price on request

Arianespace

Vega-C

European small-lift launch vehicle for polar and sun-synchronous orbit payloads up to 2,350 kg.

Payload to SSO (700 km)	2,350 kg
Payload to SSO (300 km)	~3,300 kg
First stage	P120C solid motor (shared with Ariane 6)
Second stage	Zefiro-40 solid motor
Fairing diameter	3.3 m

price on request

Astra Space designs and manufactures responsive mobile launch systems (Rocket 4.0) and flight-proven electric propulsion systems for satellites, headquartered in Alameda, California.

Astra Space

Rocket 4

Rocket 4 is Astra Space’s second-generation orbital launch vehicle, developed after the company retired the smaller Rocket 3.3 following its mixed flight record. Unlike Rocke

Height	62 ft (18.9 m)
Diameter	72 in (1.8 m)
Stages	2
Liftoff mass	~66,000 lb
First stage engines	2x Chiron (derived from Firefly Reaver), combined ~70,000-80,000 lbf thrust

$5 000 000

Chinese state-owned aviation and defense conglomerate with an emerging, narrow space-systems foray via its Chengdu subsidiary's reusable cargo spaceplane program.

Avio S.p.A. designs, manufactures, and integrates space launchers and tactical missiles, providing space propulsion solutions and the Vega rocket family for institutional, governmental, and commercial

Avio S.p.A.

Vega C

Vega C is Avio's single-body, four-stage small/medium-lift launcher, the upgraded successor to Vega, built for ESA/Arianespace to serve institutional and commercial payloads to low

Height	~35 m
Liftoff mass	~210 tonnes
Fairing diameter	3.3 m
Configuration	Single-body, 4 stages (3 solid + 1 liquid)
Stage 1 - P120C	Length 13.5 m, diameter 3.4 m, thrust 4,780 kN, ~141.4 t solid propellant

price on request

B2Space develops high-altitude balloon launch systems for deploying small satellites to near-space and low Earth orbit. The Spanish company's Nearspace Launcher platform uses stratospheric balloons to lift rockets to 40 km before ignition.

b2space

Rockoon

B2Space's Rockoon is a stratospheric balloon-assisted small satellite launch system that lifts a rocket to ~35 km altitude before ignition, cutting propellant needs and cost versus

Launch concept	Rockoon (stratospheric balloon + rocket)
Balloon release/launch altitude	~35 km
Payload capacity	Up to 200 kg
Target orbit	Low Earth Orbit, flexible orbit selection
Propellant reduction	Up to ~70% less propellant vs. conventional launchers

price on request

Heavy-lift reusable launch — New Glenn; suborbital tourism & research — New Shepard.

Blue Origin

New Glenn

New Glenn is Blue Origin's heavy-lift, partially reusable, two-stage orbital launch vehicle powered by methane-fueled BE-4 engines on its reusable first stage, capable of deliverin

Height	~98 m
Diameter	7 m
Stages	2 (reusable first stage, expendable second stage)
First stage engines	7x BE-4 (LNG/LOX methalox)
Second stage engines	2x BE-3U (LH2/LOX hydrolox)

price on request

C6 Launch Systems provides launch services and manufactures a dedicated smallsat launch vehicle for payloads up to 100 kg, offering access to all orbits.

C6 Launch Systems Inc.

C6 Launch Vehicle

C6 Launch Systems' small commercial orbital launch vehicle under development for the competitive smallsat launch market.

Target Payload	100–500 kg to LEO/SSO
Status	Development

price on request

C6 Launch Systems Inc.

C6 Rocket

Dedicated two-stage smallsat launch vehicle for payloads up to 100 kg

Height	13 meters
Diameter	1 meter
Number of stages	2
Stage 1 configuration	Three LOX-kerosene engines
Stage 2 configuration	Single LOX-kerosene engine

price on request

Chinese state launch vehicle design organisation in Beijing (CASC subsidiary); Long March 2F (crewed), LM-3B/C, LM-5/5B, LM-7, LM-8 rockets; 130+ launches from 1970; backbone of China's crewed and commercial space.

CALT (China Academy of Launch Vehicle Technology)

Long March 2C (LM-2C / CZ-2C)

The Long March 2C is a Chinese medium-lift, two-stage orbital launch vehicle developed by the China Academy of Launch Vehicle Technology (CALT). It uses storable N2O4/UDMH propella

Function	Medium-lift launch vehicle
Manufacturer	China Academy of Launch Vehicle Technology
Country of origin	China
Height	42 m (138 ft)
Diameter	3.35 m (11.0 ft)

price on request

CALT (China Academy of Launch Vehicle Technology)

Long March 3B

The Long March 3B (CZ-3B or LM-3B) is a Chinese orbital launch vehicle, the heaviest variant of the Long March 3 family, primarily used for placing communications and navigation sa

Function	Launch vehicle
Manufacturer	China Academy of Launch Vehicle Technology (CALT)
Country of origin	China
Cost per launch	US$50-70 million
Diameter	3.35 m (11.0 ft)

price on request

CALT (China Academy of Launch Vehicle Technology)

Long March 4B

The Long March 4B (LM-4B) is a Chinese three-stage expendable medium-lift launch vehicle primarily used for deploying satellites into low Earth orbit (LEO) and Sun-synchronous orbi

Function	Medium-lift launch vehicle
Manufacturer	Shanghai Academy of Spaceflight Technology
Country of origin	China
Cost per launch	US$50 million (2006)
Height	44.1 m (145 ft)

price on request

CALT (China Academy of Launch Vehicle Technology)

Long March 5

Long March 5 (CZ-5) is China's most powerful heavy-lift orbital launch vehicle, developed by CALT, capable of delivering up to 25,000 kg to LEO or 14,000 kg to GTO.

Function	Heavy-lift launch vehicle
Manufacturer	CALT
Country of origin	China
Cost per launch	~US$160 million
Height	56.97 m (186.9 ft) (standard); 63.2 m (207 ft) (extended fairing)

price on request

CALT (China Academy of Launch Vehicle Technology)

Long March 7

Chinese liquid-fuelled medium-lift launch vehicle of the Long March family, developed by CALT, used primarily to launch Tianzhou cargo spacecraft to the Tiangong space station.

Function	Medium to heavy-lift launch vehicle
Manufacturer	China Academy of Launch Vehicle Technology
Country of origin	China
Diameter	3.35 m (11 ft)
Payload to LEO - Altitude	200 km × 400 km (120 mi × 250 mi)

price on request

Chinese commercial launch company backed by CAS, developing the Kinetica rocket family for rideshare and dedicated missions, headquartered in Guangzhou.

CAS Space

Kinetica-1 (PR-1) Launch Vehicle

Chinese commercial solid-fueled medium-lift launch vehicle for LEO and SSO rideshare missions.

Propulsion	Solid
Target Orbit	LEO / SSO
Maiden Flight	2022
Missions Flown	14+
Satellites Delivered	108+

price on request

CAS Space

Kinetica-2 (PR-2) Launch Vehicle

Next-generation kerosene/LOX medium-heavy launch vehicle targeting ~6,000 kg to LEO.

Propulsion	Kerosene / LOX (Kinecore engines)
Payload to LEO	~6,000 kg
Upper Stage	Kinastra restartable stage
Status	Under development / flight testing

price on request

CASC designs and manufactures Long March launch vehicles and intercontinental strategic nuclear missiles, and provides satellite application, ground operation, financial, and internationalization serv

CASC — China Aerospace Science and Technology Corporation

Long March 2C

CASC's high-reliability medium launch vehicle with 100+ successful flights, widely used for commercial rideshare and SSO missions.

Stages	2 (plus optional upper stage)
Propellants	UDMH/N2O4 (hypergolic)
Payload to LEO	3,850 kg (200 km)
Payload to SSO	1,250 kg (700 km)
First Stage Engines	4× YF-20

price on request

CASC — China Aerospace Science and Technology Corporation

Long March 5

China's most powerful rocket, capable of 25,000 kg to LEO — used for space station modules, lunar exploration, and Mars missions.

Payload to LEO	25,000 kg
Payload to GTO	14,000 kg
Core Stage Propellants	LOX/LH2
Boosters Propellants	LOX/Kerosene (4× YF-100)
Liftoff Thrust	~1,000 tonnes

price on request

CASIC commercial launch subsidiary; Kuaizhou-1A solid quick-reaction LV (400 kg SSO) and Kuaizhou-11 (1,500 kg SSO); rapid-response launches from Jiuquan and Taiyuan.

CASIC ExPace — Kuaizhou

Kuaizhou-1A

Kuaizhou-1A is a small, quick-reaction solid-fuel launch vehicle built by CASIC's ExPace to loft light satellites to low Earth and sun-synchronous orbit from mobile transporter-ere

Stages	3 solid-propellant stages plus a liquid-propellant fourth-stage orbital adjustment module
Length	~19.4-20 m
Diameter	1.4 m (stages 1-2); 1.2 m (stages 3-4); fairing up to 1.8 m
Liftoff mass	~30 tonnes
Payload to LEO (500 km)	~300-400 kg (baseline); up to ~450 kg on enhanced variant

price on request

Celestia Aerospace offers turnkey solutions and an airborne launch platform for businesses seeking to access space, leveraging experience in nanosat projects.

Celestia Aerospace

Innovative Launch System

The Innovative Launch System is an airborne launch platform designed to provide fast, reliable, and cost-effective access to space for businesses.

Platform variants

BioPharmaSat, SemicondSat, TestSat, ClusterSat

price on request

Celestia Aerospace

Sagitarius Airborne Launch System (SALS)

Airborne launch system combining a MiG29UB jet with 2-3 stage rockets — delivers 4-16 nanosats to suborbital or orbital flight per operation.

Archer 1 operational ceiling	20 km
Space Arrow SM microgravity duration	10 minutes (suborbital)
Space Arrow CM payload to LEO	Up to 16 kg
Launch batch size	4-16 nanosats per operation

price on request

CALT/CASC commercial arm — solid Smart Dragon (Jielong) rockets for smallsat rideshare, including sea launch.

China Rocket Co. (CALT)

Long March 5 (LM-5)

China's most powerful operational rocket, capable of 25 tonnes to LEO and 14 tonnes to GTO.

Height	56.97 m
Diameter (core)	5 m
Payload to LEO	~25,000 kg
Payload to GTO	~14,000 kg
Core Propellant	LOX / LH2

price on request

Dahang Transition develops and operates medium and large reusable launch vehicles and their on-board computers, supporting satellite Internet engineering.

Cosmoleap

New Generation One-Stage Reusable Rocket

This is a new generation one-stage reusable rocket, featuring tower recovery capabilities for both land and island operations, and designed for high launch frequency and reusabilit

Launch frequency	24 rounds/year
Total annual payload capacity	150 tons/year
Recovery method	Tower recovery
Recovery sites	Both land and island
LEO capacity (recovery state)	Not less than 6.28t

price on request

Creotech Instruments is a Polish space technology company developing satellite platforms (HyperSat), spacecraft subsystems, and manufacturing services for the space industry, science, and other high-tech sectors.

Creotech Instruments S.A.

HyperSat Satellite Platform — Polish Space Electronics and Nanosatellite Systems

Creotech Instruments S.A. is a Polish space electronics company founded in 2010 in Piaseczno (near Warsaw), designing and manufacturing satellites, electronics modules, and space h

price on request

New Zealand and Netherlands aerospace company developing the Mk-II Aurora reusable spaceplane and refuellable in-space propulsion systems for satellite missions.

Dawn Aerospace

AURORA SPACEPLANE

Aurora is a remotely piloted suborbital spaceplane that combines rocket performance with aircraft reliability to provide routine, affordable access to suborbital space and speeds o

Top Speed	Mach 3.7
Max Altitude	100 km
Turnaround Time	4 hr
Max Payload Weight	15 kg (33 lbs)
Suborbital Profile Max Alt	100+ km

price on request

Private Chinese reusable launcher — Nebula-1 (~2 t to LEO) nearing first orbital flight; larger Nebula-2 in development.

Deep Blue Aerospace

Nebula-1

Reusable, kerolox orbital launch vehicle with VTVL first-stage recovery; ~2,000 kg to LEO.

Propellant	Kerosene / liquid oxygen (kerolox)
Configuration	Two-stage, reusable first stage (VTVL)
Payload to LEO	~2,000 kg
Height	~30.2 m (orbital variant, Nebula-1A)
Diameter	3.35 m (first stage)

price on request

European defence manufacturer focused on scalable strike and air-defence systems for European and allied armed forces.

Destinus

Ruta Block 2

Extended-range cruise system for precision strike against hardened and high-value targets at 700+ km.

Range	700+ km
Payload	250 kg
Guidance	EO/IR seeker with AI-assisted target recognition
Navigation	Low-altitude terrain-following, GNSS-denied capable
Launch	Booster-assisted salvo from 40 ft container

price on request

Satellite component and subsystem manufacturer producing control systems, telemetry, optical payloads, propulsion, power systems, and multi-band transceivers for LEO and MEO satellite missions.

US manufacturer of non-explosive actuators (TiNi FrangiBolt, pin pullers, ejectors) and energetic hold-down and release systems.

Ensign-Bickford Aerospace & Defense (EBAD)

Flight Termination Systems

EBAD Flight Termination Systems (FTS) provide range safety assurance for launch vehicles and missiles by delivering redundant explosive assemblies capable of terminating flight whe

Type	Flight Termination System (FTS)
Components	ESAD, FCDCA transfer lines, destruct charges (bulk, linear, bi-directional, conical)
Redundancy	Redundant explosive assemblies
Applications	Launch vehicles, tactical missiles, hypersonics, strategic missiles
System role	Range safety — vehicle destruction on wayward flight

price on request

Singapore-based developer of hybrid-propulsion, explosives-free small-satellite launch vehicles and sounding rockets.

Equatorial Space Systems

DORADO Sounding Rocket

Responsive, 100% explosives-free hybrid-propulsion suborbital sounding rocket delivering 20 kg to 100 km apogee.

Propulsion	Hybrid HTP oxidizer / HRF-1 fuel
Payload capacity	20 kg
Apogee	100 km
Microgravity access	~3 minutes
Payload volume	41 L

price on request

Equatorial Space Systems

VOLANS Launch Vehicle

Modular, low-cost, 100% pyrotechnics-and-explosives-free hybrid-propulsion launch vehicle carrying up to 750 kg to LEO.

Propulsion	Hybrid HTP oxidizer / HRF-1 fuel
Payload capacity	Up to 750 kg (simulated for 400 km, 40° orbit)
Fairing length (main)	2.40 m
Fairing length (total)	4.77 m
Fairing diameter	21.80 m

price on request

Indian reusable launch vehicle startup — developing Razor Crest Mk 1 (RCM1), a fully reusable medium-lift rocket capable of 16 orbital insertions per flight, operating India's largest private rocket test facility.

EtherealX (Ethereal Exploration Guild)

Razor Crest Mk 1 (RCM1) Reusable Medium-Lift Launch Vehicle

Fully reusable medium-lift launch vehicle from EtherealX — up to 16 orbital insertions per flight, 72–96hr turnaround, profitable even when not fully loaded. India's largest privat

Vehicle type	Fully reusable medium-lift launch vehicle
Orbital insertions per flight	Up to 16 (multi-orbit rideshare)
Turnaround time	72–96 hours
Configurations	Expendable / Partially Reusable / Fully Reusable
Economics	Profitable even at partial load capacity

price on request

Alpha small-lift rocket; lunar lander Blue Ghost; Medium Launch Vehicle in development with NG.

Firefly Aerospace

Alpha

Firefly's small-lift orbital launch vehicle delivering up to 1,000 kg to LEO on a dedicated or rideshare basis.

Payload to LEO (200 km)	1,000 kg
Payload to SSO (500 km)	630 kg
First stage engines	4× Reaver (RP-1 / LOX)
Second stage engine	1× Lightning (RP-1 / LOX, vacuum-optimized)
Height	29 m

price on requestdatasheet

Firefly Aerospace

Medium Launch Vehicle (MLV)

Firefly's medium-lift launch vehicle in development, targeting 16,000 kg to LEO using Miranda engines co-developed with Northrop Grumman.

Payload to LEO	~16,000 kg
Engines	Miranda (LOX / RP-1, oxidizer-rich staged combustion)
Development partner	Northrop Grumman
Launch site	Cape Canaveral Space Force Station, Florida (planned)
Status	In development

price on request

Chinese commercial launch company; Ceres-1 solid small LV (first flight Nov 2020) and Pallas-1 liquid medium LV in development; multiple successful commercial orbital launches.

Galactic Energy

Ceres-1

Galactic Energy's four-stage solid-fuel commercial small launch vehicle delivering 300 kg to SSO from Chinese spaceports.

Stages	4 (all solid)
Payload to LEO	~400 kg
Payload to SSO	~300 kg (500 km)
First Flight	November 7, 2020 (success)
Achievement	First Chinese private company to orbit on first attempt

price on request

Gilmour Space Technologies builds and operates an integrated launch vehicle, satellite platform, and spaceport for commercial, government, and defence customers.

Gilmour Space Technologies

Eris

Gilmour Space's three-stage launch vehicle with hybrid upper stages, targeting 305 kg to SSO from Queensland, Australia.

Stages	3
Stage 1 Propellants	LOX/Kerosene
Stage 2/3 Propellants	Hybrid (liquid oxidizer / solid fuel)
Payload to SSO	305 kg at 500 km
Launch Site	Bowen Orbital Spaceport, Queensland, Australia

price on request

GK Launch Services provides commercial launch services using Soyuz rockets from Baikonur Cosmodrome, offering dedicated and rideshare missions to LEO, SSO, and GTO orbits.

GK Launch Services

Soyuz-2

Soyuz-2 is a series of Russian expendable medium-lift launch vehicles, representing the seventh major iteration of the Soyuz rocket family, featuring upgraded engines and a digital

Function	Medium-lift launch vehicle
Manufacturer	RKTs Progress
Country of origin	Russia
Cost per launch	US$35 million (2018, 2.1b without fourth stage)
Height	46.3 m (152 ft)

price on requestdatasheet

GK Launch Services

Soyuz-2.1a

Modernized medium-lift Soyuz launch vehicle with digital flight control, flown from Baikonur, Plesetsk and Vostochny.

Stages	3 (4 liquid boosters + core + third stage); optional Fregat upper stage
Height	46.3 m
Diameter	2.95 m (core); 10.3 m booster span
Launch mass	~312,000 kg
Propellant	RP-1 / LOX (all stages)

price on requestdatasheet

Glavkosmos coordinates international human spaceflight projects, facilitates satellite launches, develops and supplies rocket components, and provides equipment for space crews.

Glavkosmos

Ejection System

The Ejection System is designed to deliver compressed air to protect the lower part of a Launch Vehicle (LV) body from high-temperature plumes during engine operation.

Purpose	Compressed air delivery in nominal mode for LV body lower part protection against high-tem
Year of release	Development start 2002
Flight qualification of the product	No
Possibility to adapt the product to customer requirements	Yes

price on request

Glavkosmos

Fairing

The Fairing is a head fairing designed to protect spacecraft and upper stages from aerodynamic and thermal loads during a launch vehicle's ascent through dense atmospheric layers.

Purpose	Design and manufacture of head fairings for the protection of spacecraft and upper stage f
Flight qualification of the product	Yes
Brief history of flight qualification	HF 1.750 for Soyuz launch vehicle (Ø 3715 mm, length 8450 mm) with upper stage "Fregat". M
Possibility to adapt the product to customer requirements	Yes
HF RBF 1.750 for the Soyuz launch vehicle	Ø 3715 mm, length 8450 mm

price on request

Glavkosmos

Transition Compartment

The Transition Compartment is a structural component for launch vehicles, designed to ensure the docking of the space head with the previous stage block and the installation of the

Purpose	Design and manufacture of transition compartments to ensure the docking of the space head
Flight qualification of the product	Yes
Brief history of flight qualification	Transition compartment for use with HF (Ø 4110 mm, length 11433 mm) and LV "Soyuz-2". Adap
Possibility to adapt the product to customer requirements	Yes
Transition compartment 14C227	Ø 3715 mm, length 8450 mm or 10400 mm

price on request

Glavkosmos

Universal Upper Stage “Fregat”

The Fregat Universal Upper Stage is designed to serve as the third stage of launch vehicles, enabling the placement of various satellites into different orbits. It has a flight-qua

Purpose	Design and manufacture of upper stage for use as the 3rd stage of the launch vehicle and l
Flight qualification of the product	Yes
Brief history of flight qualification	Upper stage "Fregat", upper stage "Fregat-MT", upper stage "Fregat - SB".
Possibility to adapt the product to customer requirements	Yes
Initial mass with maximum dressing, kg	6235/7640/11680

price on requestdatasheet

French hybrid rocket propulsion company developing the OB1 microlauncher (235 kg to LEO) with patented annular combustion chamber technology.

HyPrSpace

Hype

HyPrSpace's hybrid-propellant small launch vehicle targeting 50 kg to SSO from a European spaceport.

Propulsion	Hybrid (LOX / solid fuel)
Payload to SSO	~50 kg
Target Orbit	Sun-synchronous
Country	France

price on request

HyPrSpace

Orbital Baguette One

OB-1 is HyPrSpace's orbital micro-launcher under development in France, using a turbopump-free hybrid rocket engine to deliver up to 235 kg of payload to low Earth orbit.

Height	~16 m
Propulsion	Hybrid rocket engine ('Terminator'): solid HDPE fuel grain + liquid oxidizer, helium-press
Engine thrust (demonstrator)	~100 kN
Payload to LEO	Up to 235-250 kg
Target orbit	LEO, up to ~400 km altitude

price on request

Malaysian NewSpace launch and re-entry services company developing the DNLV (Domino Next Launch Vehicle) — Malaysia's first commercially developed orbital small launch vehicle — and the MERCAP microgravity experimental re-entry capsule.

South Korean developer of hybrid-propulsion small satellite launch vehicles, offering dedicated orbital launches from 90 kg to 1,300 kg to SSO.

INNOSPACE

BLACK BIRD Sounding Rocket Series

Customer-configurable hybrid-propulsion sounding rockets for microgravity and atmospheric research, using liquid nitrous oxide (LN₂O) and HDPE propellants.

BLACK BIRD-1 — Length	1,485 mm
BLACK BIRD-1 — Diameter	105 mm
BLACK BIRD-1 — Mass	8.5 kg
BLACK BIRD-1 — Payload	1 kg
BLACK BIRD-1 — Apogee	~1 km

price on request

INNOSPACE

HANBIT-Micro Launch Vehicle

Two-stage + kick stage small satellite launcher delivering up to 170 kg to 500 km SSO, with dual methane upper-stage engines and a precision kick stage.

Payload capacity	170 kg (500 km SSO)
Height	22.5 m
Diameter	1.4 m
Target orbit	500 km SSO
Stage 1 engine	1× 245 kN hybrid (paraffin/LOx), 130 sec burn

price on request

INNOSPACE

HANBIT-Mini Launch Vehicle

Three-stage small satellite launcher delivering up to 1,300 kg to 500 km SSO, powered by nine 25-ton hybrid engines in the first stage.

Payload capacity	1,300 kg (500 km SSO)
Height	39.6 m
Diameter	3.7 m
Stage 1 engines	9× 245 kN hybrid (paraffin/LOx)
Stage 1 total thrust	~2,205 kN

price on request

INNOSPACE

HANBIT-Nano Launch Vehicle

Two-stage hybrid-propulsion small satellite launch vehicle delivering up to 90 kg to 500 km SSO, with HyPER hybrid and LiMER methane upper-stage variants.

Payload capacity	90 kg (500 km SSO)
Height	21.7 m
Diameter	1.4 m
Target orbit	500 km SSO
Stage 1 engine thrust	245 kN (25 ton-class hybrid)

price on request

Japanese aerospace startup developing ASCA, a reusable single-stage-to-orbit launch vehicle targeting daily space transportation with turnarounds of once per day and 1,000+ repeat flights.

Innovative Space Carrier (ISC)

ASCA Reusable Launch Vehicle

Single-stage-to-orbit reusable rocket designed for daily orbital operations — 10-tonne payload to 400 km LEO, 50-passenger capacity, 1,000+ reuse flights, once-per-day turnaround.

Vehicle Type	Single-Stage-to-Orbit (SSTO), Reusable
Payload to LEO (400 km)	10,000 kg
Passenger Capacity	50
Reuse Lifetime	>1,000 flights
Turnaround Time	1 day (target)

price on request

US private aerospace company developing the NEPTUNE and TRITON low-cost orbital launch vehicles, TubeSat and CubeSat personal satellite kits, a commercial LunarStation lander, and orbital tourism expeditions.

Interorbital Systems

NEPTUNE_100 / TRITON_4500 Launch Vehicles

Small-lift and medium-lift two-stage orbital launch vehicles using storable bipropellant — NEPTUNE_100 (100kg payload) and TRITON_4500 (4,500kg payload) to 500km polar orbit.

NEPTUNE_100 payload	100 kg to 500 km polar orbit
TRITON_4500 payload	4,500 kg to 500 km polar orbit
Propellants	White Fuming Nitric Acid (WFNA) + Turpentine
Engine cooling	Ablative (filament-wound composite)
Max engine burn time	40 minutes

price on request

Interorbital Systems

NEPTUNE_100 Launch Vehicle

Low-cost small-lift two-stage orbital rocket delivering 100 kg to 500-km polar orbit at $599,999 per dedicated launch.

Vehicle class	Small-lift orbital
Stages	2
Payload to 500 km polar orbit	100 kg
Dedicated launch price	$599,999
Price per kg to orbit	$4,918/kg

$599 999

Interorbital Systems

TRITON_4500 Launch Vehicle

Medium-lift two-stage orbital launch vehicle delivering up to 4,500 kg to 500-km polar orbit at $12M per dedicated launch.

Vehicle class	Medium-lift orbital
Stages	2
Payload to 500 km polar orbit	4,500 kg
Dedicated launch price	$12,000,000
Price per kg to orbit	$2,667/kg

$12 000 000

Interstellar Technologies designs and manufactures orbital launch vehicles and satellite communication systems, aiming to provide space infrastructure.

Interstellar Technologies

MOMO / ZERO Sounding Rockets

Interstellar Technologies' commercial sounding rockets — MOMO (suborbital) and ZERO (orbital target) — launched from Taiki, Hokkaido Japan.

MOMO Type	Single-stage suborbital
MOMO Propellants	Ethanol/LOX
MOMO Altitude	>100 km (above Kármán line)
ZERO Payload to SSO	~150 kg (target)
Launch Site	Taiki-cho, Hokkaido, Japan (private)

price on requestdatasheet

iRocket designs and manufactures next-generation reusable small launch vehicles and provides advanced propulsion technology for aerospace and defense applications.

iRocket

Shockwave

Fully autonomous, two-stage, 100%-reusable launch vehicle targeting 300-1,500 kg payloads to LEO/GEO with 24-hour turnaround.

Configuration	Two-stage-to-orbit, vertical takeoff / vertical landing (VTVL)
Height	~125 ft (~38 m)
Diameter	9 ft (~2.7 m)
Payload capacity	300-1,500 kg to LEO
Target orbits	LEO, GEO, translunar

price on request

Isar Aerospace designs and manufactures the 'Spectrum' two-stage launch vehicle for small and medium satellites and constellations, providing launch services to global customers.

Isar Aerospace

Spectrum

Isar Aerospace's two-stage orbital launch vehicle targeting 1,000 kg to LEO using LOX/propane, launching from Andøya Space Center in Norway.

Stages	2
Propellants	LOX/Propane
First Stage Engines	9× Aquila
Payload to LEO	~1,000 kg
Payload to SSO	~700 kg

price on request

Chinese commercial launch company; Hyperbola-1 first private orbital success July 2019; Hyperbola-2 reusable liquid LV in development; founded 2016, Beijing.

iSpace (Beijing Interstellar Glory)

Hyperbola-1

Hyperbola-1 (SQX-1) is a four-stage, all-solid-propellant small-lift launch vehicle developed by iSpace; its July 2019 maiden flight made it the first Chinese private company to su

Height	20.8 m
Diameter	1.4 m
Liftoff mass	~31 tonnes
Stages	4 (all solid-fuel stages with liquid-fuel attitude control on upper stage)
Payload to LEO	~300 kg

$5 000 000

Japan Aerospace Exploration Agency (JAXA) is Japan national aerospace and space agency, responsible for research, technology development, and launch of satellites and space missions.

JAXA - Japan Aerospace Exploration Agency

Epsilon Launch Vehicle

The Epsilon is a solid-propellant launch vehicle developed by JAXA to provide cost-effective and flexible access to space for small satellites and scientific payloads. Derived from

Height	26
Mass	95.4
Diameter	2.6
Payload to LEO	1200
Stages	3 solid + optional liquid

price on request

JAXA - Japan Aerospace Exploration Agency

H-IIA Launch Vehicle

The H-IIA is Japan workhorse liquid-propellant launch vehicle, developed by JAXA and operated by Mitsubishi Heavy Industries since 2001. Built on heritage from the H-II rocket, the

Height	53
Liftoff mass	289
Payload to GTO	4.0
Payload to LEO	10.0
First stage engines	2 LE-7A

price on request

JAXA - Japan Aerospace Exploration Agency

H3 Launch Vehicle

The H3 is Japan new flagship launch vehicle developed by JAXA and Mitsubishi Heavy Industries. Designed to replace the H-IIA, the H3 offers improved cost efficiency, flexibility, a

Height	63
Liftoff mass	574
Payload to GTO	6.5
Payload to SSO	4.0
First stage engines	2-3 LE-9

price on request

LandSpace is a space transportation company founded in 2015, specializing in the development, manufacturing, testing, and launching of medium and large reusable liquid oxygen-methane launch vehicles.

LandSpace

Zhuque-2 (LOX/Methane)

LandSpace's LOX/methane launch vehicle — the world's first methane-fueled rocket to reach orbit, achieving success on its third flight in July 2023.

Propellants	LOX/Methane (both stages)
First Stage Engines	4× TQ-12
Payload to LEO	~6,000 kg
Payload to SSO	~4,000 kg
Historical Achievement	World's first methane-fueled rocket to reach orbit (July 12, 2023)

price on request

LandSpace

Zhuque-3 (Reusable Medium Launch Vehicle)

LandSpace's fully reusable medium launch vehicle under development, targeting 21,000 kg to LEO using its Tianque-12 LOX/methane engine.

Propellants	LOX/Liquid Methane (LCH4)
First Stage Engines	9× Tianque-12 (~1,000 kN each)
Payload to LEO	~21,000 kg (reusable configuration)
Reuse Method	Propulsive landing (both stages)
Predecessor	Zhuque-2 — world's first methane rocket to orbit (July 2023)

price on request

Latitude designs and manufactures a multi-configurable launcher in France for dedicated SmallSat launch services, offering frequent and affordable access to orbit.

Latitude

Zephyr

Latitude's small orbital launch vehicle targeting 100+ kg to SSO from Guiana Space Centre, powered by a LOX/methane propulsion system.

Stages	2
Propellants	LOX/Methane (both stages)
Engine	Navier (in-house, additive manufactured)
Payload to SSO	~100 kg
Launch Site	Guiana Space Centre, Kourou

price on request

LinkSpace (翎客航天) is China's first private reusable rocket company, developing VTVL launch vehicles and liquid rocket engines.

LinkSpace

NewLine-1

LinkSpace's orbital-class reusable launch vehicle, targeting small commercial satellite launches to sun-synchronous orbit with a reusable first stage rated for 10+ launches.

Height	24 m
Diameter	1.8 m
Payload to orbit	200 kg
Target orbit	500 km SSO (sun-synchronous)
Take-off weight	42 t

price on request

LinkSpace

RLV-T Series

Family of VTVL (vertical take-off, vertical-landing) reusable rocket test vehicles used by LinkSpace to develop and validate its reusability technology.

Prototypes developed	RLV-T1 - RLV-T5
Test flights conducted	300+
Wind tolerance for soft landing	up to 10 m/s
Engine thrust variability	20%-100% (variable thrust)
Total engine ignition time	30,000+ seconds

price on request

LinkSpace

RLV-T5 (NewLine Baby)

Sub-scale VTVL reusable rocket technology demonstrator used by LinkSpace to validate powered descent and precision vertical landing.

Height	8.1 m
Diameter	0.65 m
Liftoff mass	1.5 metric tons
Propulsion	5x variable-thrust ethanol / liquid-oxygen engines
Max altitude achieved	300.2 m (Aug 9, 2019 flight)

price on request

LinkSpace

SRV-1 (RLV-T6)

China's first suborbital reusable vehicle (test code RLV-T6), a multi-purpose LOX/methane VTVL rocket for microgravity, atmospheric and payload testing missions.

Test designation	RLV-T6
Diameter	1.2 m
Height	15 m
Take-off weight	8.5 t
Propellant	LOX / Methane

price on request

Formerly ABL Space Systems; now Long Wall, developing containerized missile defense systems, hypersonic test vehicles, and the RSX liquid booster, building on its RS1 orbital launch vehicle heritage.

Long Wall Space (formerly ABL Space Systems)

RSX

RSX is Long Wall’s small launch vehicle, carrying years of design iteration, subsystem testing, and flight operations experience derived from ABL Space Systems’ RS1 pro

price on request

Canadian global aerospace manufacturer delivering complex aeroengine and aerostructure assemblies, Black Brant sounding rockets, and small satellite bus platforms for civil and defence markets worldwide.

Magellan Aerospace

Black Brant Sounding Rocket

Family of solid-propellant sounding rockets launching scientific payloads since 1962 — 70–850 kg payload, 150–1,500+ km altitude, >98% mission success rate, 1,000+ launches.

Payload Capacity	70–850 kg
Altitude Range	150–1,500+ km
Mission Success Rate	>98%
Total Launches	>1,000
Propellant	Aluminized HTPB solid propellant

price on request

MaiaSpace designs, manufactures, operates, and commercializes reusable mini launchers and space mobility solutions for various orbits, serving customers like Eutelsat.

MaiaSpace

Maia

Maia is MaiaSpace's two-stage, methane/oxygen orbital launcher, billed as Europe's first reusable, eco-responsible mini launcher, designed to serve LEO/SSO smallsat constellations

Height	50 m
Diameter	3.5 m
Stages	2 stages (plus optional Colibri third stage/kick stage)
First stage engines	3x Prometheus engines
Second stage engines	1x Prometheus engine (re-ignitable)

price on request

RocketStar is a U.S. aerospace technology company developing reusable aerospike rocket engines, water-fueled and fusion-enhanced electric propulsion for spacecraft, and a suite of digital signal processing (DSP) software for secure communic

Miles Space / RocketStar

Cowbell Suborbital Test Rocket

12-meter aerospike-powered developmental suborbital test rocket intended to fly from Cape Canaveral's Launch Complex 48.

Length	12 meters
Target test altitude	~21,000 meters (suborbital)
Propulsion	RocketStar Aerospike Engine
Launch site	Launch Complex 48, Cape Canaveral, Florida
Vehicle class	Single-stage-to-orbit (SSTO) developmental test rocket

price on request

Miles Space / RocketStar

RocketStar Aerospike Engine

Patent-pending 3D-printed aerospike rocket engine producing 25-35% more thrust than conventional bell-cone engines with built-in thrust vectoring.

Thrust gain vs. bell-cone	25-35% more thrust, no extra fuel
Performance gain	~20% better than conventional rocket engines
Thrust vectoring	Individually controlled combustion chambers; no gimbals/actuators needed
Altitude compensation	Adjusts to changing atmospheric pressure at any altitude
Manufacturing	3D-printed, patent-pending design

price on request

H3 next-generation Japanese launch vehicle (heir to H-IIA); commercial GTO/SSO missions.

Mitsubishi Heavy Industries Launch Services

H-IIB

Japan's retired heavy-lift launch vehicle used exclusively to launch the HTV (Kōnotori) cargo spacecraft to the ISS, with a perfect 9-for-9 success record.

Payload to LEO	19,000 kg
Payload to ISS orbit	16,500 kg
Height	56.6 m
First Stage Diameter	5.2 m
Launch Mass	531,000 kg

price on request

Nammo is an aerospace and defense company that designs and manufactures rocket motors for military and space applications, ammunition, and shoulder-launched munitions systems.

Nammo

M-10 / DM-1650 Solid Rocket Booster Motors for Ariane 5 and Ariane 6

Nammo (Nordic Ammunition Group) is a Norwegian-Finnish defense and aerospace company headquartered in Raufoss, Norway, specializing in solid rocket propulsion and ammunition. In th

price on request

ISRO's primary commercial arm; manages PSLV/SSLV production, provides international launch services, and facilitates Indian private space industry growth.

NewSpace India Limited (NSIL)

PSLV

The Polar Satellite Launch Vehicle (PSLV) is ISRO's proven four-stage workhorse rocket, commercially marketed by NewSpace India Limited (NSIL) for launching satellites into sun-syn

Height	44 m
Core diameter	2.8 m
Stages	4 stages, alternating solid and liquid propulsion
Lift-off mass (PSLV-XL)	320,000 kg
Payload to LEO (PSLV-XL, 200 km)	3,800 kg

price on requestdatasheet

Minotaur family, Pegasus XL, Antares (legacy); MLV co-development with Firefly.

Northrop Grumman Space Systems

Antares 330

Antares 330 is Northrop Grumman's next-generation, two-stage expendable rocket designed to launch Cygnus cargo spacecraft to the ISS, replacing the retired Antares 230+ with a new

Stages	Two-stage: liquid-fueled first stage + solid-fueled second stage
First stage engines	7x Firefly Aerospace Miranda engines (RP-1/LOX)
First stage thrust	~7,200 kN combined
Second stage	Castor 30XL solid rocket motor
Diameter	3.9 m (payload fairing / core)

price on request

Omspace Rocket and Exploration designs and manufactures reusable rockets for small and nano satellites, operating from Ahmedabad, Gujarat, India.

Omspace Rocket and Exploration

Infinity One

Infinity One is a reusable launch vehicle designed for dedicated, on-demand orbital insertion of small payloads to Low Earth Orbit.

price on request

Omspace Rocket and Exploration

INFINITY ONE REUSABLE ROCKET (Project AROM – Sounding Rocket)

INFINITY ONE is a reusable rocket designed for launching small and nano satellites, offering affordability, reliability, and efficiency for space exploration and commercial venture

Payload Capacity	500 Kgs
Reach	upto 500 kms

price on request

Chinese private launch-vehicle developer building the OS-X suborbital and OS-M orbital solid-fuel rocket families, and China's first privately funded company authorized to develop and manufacture launch vehicles.

OneSpace Technologies

OS-M Orbital Launch Vehicle

Four-stage solid-fuel orbital small-satellite launcher targeting sun-synchronous orbit.

price on request

OneSpace Technologies

OS-X Suborbital Sounding Rocket

Solid-fuel suborbital sounding rocket family; OS-X0 was China's first privately developed commercial suborbital rocket to fly.

price on request

Chinese commercial launch company developing the Gravity Series medium and heavy-lift rockets, headquartered in Yantai, Shandong.

Orienspace (Orient Space)

Gravity-1

Orienspace's solid-fuel heavy launch vehicle — the world's most powerful solid rocket — delivering 6,500 kg to SSO from sea launch in January 2024.

Propulsion	All solid (4× CAS-250 first stage)
Payload to SSO	6,500 kg (500 km)
Payload to LEO	~14,000 kg
First Flight	January 11, 2024 (success from sea launch)
Achievement	World's most powerful solid-fuel rocket; world record solid rocket payload to orbit

price on request

Orienspace (Orient Space)

Gravity-1 Launch Vehicle

World-record solid-fueled heavy launcher with bundled stage design, supporting sea and land launches.

Target Orbit	SSO / LEO
Payload to 500 km SSO	~6,000 kg
First Stage	4× solid motor (bundled)
Upper Stage	Liquid-fueled
Launch Mode	Sea launch / Land launch

price on request

PacSci EMC designs and manufactures mission-critical pyrotechnic and energetic material devices and integrated systems for aerospace, defense, energy and space applications.

PacSci EMC

Flight Termination System

The Flight Termination System (FTS) is a safety-critical product designed to prevent inadvertent initiation of a destruct sequence and to terminate the flight of missiles, rockets,

Redundant Ordnance events	5
Interface	High Speed serial Bus with Mission Computer
Fiber Optic Optical Block Compliance	MIL-STD-1901A
Sequencer Assembly Qualification	MIL-STD-1901A
Flight Termination Assembly Qualification	RCC319

price on requestdatasheet

South Korean small launch vehicle company developing the liquid-methane Blue Whale rocket family and in-house propulsion systems.

Perigee Aerospace

Blue Whale 0.1

Educational sounding rocket - South Korea's first civilian liquid-propellant rocket.

Vehicle type	Educational sounding rocket
Height	3.2 m
Diameter	190 mm
Launch mass	52 kg
Propulsion	Pressure-fed LOX/Ethanol

price on request

Perigee Aerospace

Blue Whale 0.4

Suborbital research vehicle for microgravity payloads and technology demonstrations.

Vehicle type	Suborbital research vehicle
Height	7.5 m
Diameter	760 mm
Launch mass	800 kg
Payload capacity	20 kg to suborbital trajectory

price on request

Perigee Aerospace

Blue Whale 1

Two-stage orbital launch vehicle delivering up to 200 kg to 500 km SSO.

Vehicle type	Two-stage orbital launch vehicle
Height	21 m
Diameter	1,600 mm
Launch mass	19,800 kg
Payload capacity	Up to 200 kg to 500 km SSO

price on request

Phantom Space Corporation provides satellite manufacturing, launch services, and develops data constellations, with a focus on revolutionizing space commerce.

Phantom Space

Daytona

Phantom Space's small orbital launch vehicle targeting 450 kg to LEO using liquid propellants with a focus on high launch cadence at low cost.

Payload to LEO	~450 kg
Propellants	LOX/Kerosene
Target Price	$2–3M per launch
HQ	Tucson, Arizona, USA
Status	Development

price on request

Brazilian NewSpace startup building PocketQube/CubeSat nanosatellites, sounding rockets, and STEM space-education programs to democratize access to space.

PION Labs

PION Educational Satellite Launcher (PESL)

The PION Educational Satellite Launcher (PESL) is a suborbital rocket developed by PION Labs, designed to carry educational satellites like CanSats and CubeSats.

Launch Site	Centro de Lançamento da Barreira do Inferno (CLBI), Rio Grande do Norte
Payload Capacity	Seven payloads (CanSat and CubeSat formats)
Maximum Altitude	3,000 meters
Recovery Method	Parachute deployment, sea recovery

price on request

Miura 5 partially-reusable small-lift rocket; suborbital Miura 1 — first European commercial reusable launcher.

PLD Space

Miura 1

Miura 1 is PLD Space's single-stage, reusable suborbital sounding rocket that became the first privately developed European rocket to reach space on 7 October 2023.

Length	12.5 m
Diameter	0.7 m
Stages	1
Structure material	Aluminium 2014 Series, monohull
Mass at liftoff	2,620 kg

price on request

PLD Space

Miura 5

Miura 5 is PLD Space's two-stage, reusable orbital launch vehicle for small satellites, currently in development to offer dedicated, rideshare and piggyback launch services at high

Height	35.7 m
Diameter	2 m
Stages	2 stages + optional kick stage
Propellant	Biokerosene (RP-1) + Liquid Oxygen
Structural material	Aluminium 2014 / Composite (CFRP)

price on request

German developer of reusable, horizontal-takeoff-and-landing spaceplanes for orbital launch and hypersonic transport.

POLARIS Raumflugzeuge

Aurora Light Spaceplane

Aurora is POLARIS Raumflugzeuge's flagship two-stage, fully reusable spaceplane, designed for aircraft-like runway operations to deliver small/medium satellites to orbit and suppor

Length	~28 meters
Stages	Two-stage (reusable turbofan+aerospike main stage; rocket-powered upper stage)
Orbital payload capacity	1,000 kg to low Earth orbit
Suborbital payload capacity	up to 10,000 kg
Peak altitude	>100 km

price on request

POLARIS Raumflugzeuge

Future Heavy Spaceplane

Roadmap concept for a fully reusable heavy orbital spaceplane, evolving step-by-step toward a single-stage-to-orbit (SSTO) vehicle.

Target timeframe	Early 2030s
Configuration	Semi-SSTO ('1.5-stage'), evolving toward full SSTO
Target cost reduction	At least an order of magnitude vs. traditional rockets
Applications	Crew/cargo transport, satellite launch, debris removal, lunar/interplanetary payloads (wit
TRL	2-3 (concept/roadmap stage)

price on request

POLARIS Raumflugzeuge

Spaceplane Aerial Refueling System

Optional aerial-refueling capability for POLARIS spaceplanes and hypersonic aircraft, plus dedicated uncrewed tanker aircraft.

Refuel media	Kerosene, potentially liquid oxygen
Program sponsor	BAAINBw (since 2024)
Demonstrators	ALEDA (simulated tanker), Mini MIRA II (receiver), ORCA (scaled tanker, in manufacturing)
Flight heritage	Numerous fully automated formation test flights completed
TRL	5 (formation test flights conducted, tanker demonstrator in manufacturing)

price on request

POLARIS Raumflugzeuge

VEGA

VEGA is a fully reusable, two-stage, horizontally launched spaceplane designed as a hypersonic testbed that can also serve as a small-satellite launcher.

Configuration	Two-stage, fully reusable, horizontal launch
Primary role	Hypersonic research and experimental testbed
Secondary role	Small-satellite launcher (with expendable upper stage)
Program sponsor	German Federal Office of Bundeswehr Equipment (BAAINBw)
TRL	4-5 (design contract awarded, follow-on manufacturing/flight-test options)

price on request

Ukrainian small-launch startup developing Promin 1 (Zaarbird), an ultra-light autophagic rocket that burns its own solid-fuel airframe to orbit pico- and nanosatellites.

Promin Aerospace

Promin 1 (Zaarbird)

Ultra-light autophagic small-satellite launch vehicle carrying pico/nanosatellite payloads to orbit.

Vehicle mass (approx.)	~100 kg
Payload class	Pico/nanosatellites, target ~0.1-3 kg to LEO (launcher family spans 100-500 kg mass class)
Propulsion technology	Autophagic (self-devouring) solid-fuel engine; fuel tank doubles as airframe, gasified and
Orbital debris	Designed to leave no spent stage/tank structure in orbit
Turnaround time	As little as ~1 month from order to launch (company target)

price on request

Radian Aerospace designs and manufactures fully-reusable orbital mission platforms and reentry vehicles for routine and affordable space access.

Radian Aerospace

Radian One

Radian One is a planned single-stage-to-orbit, fully reusable spaceplane designed for rapid, on-demand access to Low Earth Orbit from compatible runways.

Reusability	Fully reusable for up to 100 missions
On-demand capability	90-minute
Turnaround between flights	48-hour
Downmass capability	Industry-leading
Applications	Dual-use

price on request

Reaction Dynamics designs and manufactures hybrid rockets, including the RDX Aurora, for small satellite launch services, aiming for cost-effective and reliable access to Low Earth Orbit.

Reaction Dynamics

Aurora

Aurora is a two-stage hybrid rocket designed to provide responsive, on-demand, and affordable launch capabilities for small satellites, ensuring sovereign and ITAR-free space acces

Powered by	RE-202C
Payload capacity	up to 200kg

price on request

Relativity Space builds reusable medium-to-heavy-lift rockets, such as the Terran R, to provide access to space for a range of customers including companies and government entities.

Relativity Space

Terran 1

Relativity Space's debut orbital launch vehicle — the world's first 3D-printed rocket — retired after its inaugural flight attempt in March 2023.

Height	33.5 m
Propellants	LOX/Liquid Methane (LNG)
First Stage Engines	9× Aeon 1
Payload to LEO	1,250 kg (designed)
Manufacturing	85%+ mass 3D-printed (Stargate printers)

price on request

Relativity Space

Terran R

Relativity Space's fully reusable medium launch vehicle — both stages land and fly again — targeting 20,000 kg to LEO with 3D-printed airframe.

Stages	2 (both reusable, propulsive landing)
Propellants	LOX/Liquid Methane
Engines	Aeon R (first stage cluster + upper stage)
Payload to LEO	~20,000 kg (reusable)
Manufacturing	3D-printed airframe (Relativity Stargate printers)

price on request

German launch company developing RFA ONE small satellite launch vehicle with staged-combustion Helix engines and Redshift OTV for last-mile delivery.

Rocket Factory Augsburg

RFA ONE

RFA ONE is a German three-stage small-lift orbital launch vehicle developed by Rocket Factory Augsburg to deliver payloads of up to about 1,600 kg to LEO.

Height	30 m
Diameter	2 m
Stages	3 (first stage, second stage, Redshift orbital transfer third stage)
First stage engines	9x Helix engines, ~900 kN total, RP-1/LOX, staged combustion
Second stage engine	1x Helix Vac, RP-1/LOX, Isp ~350 s

price on request

Dedicated small-satellite launches to LEO/SSO via Electron; Neutron medium-lift in development.

Rocket Lab

Electron

Electron is an expendable, two-stage orbital launch vehicle developed and operated by Rocket Lab, designed to deliver small satellites to LEO and SSO on dedicated, frequent, low-co

Height	18 m
Diameter	1.2 m
Mass	13.0 t
Stages	2 (plus optional Curie kick stage)
First stage engines	9x Rutherford (electric pump-fed, RP-1/LOX)

price on requestdatasheet

Rocket Lab

Neutron

Neutron is Rocket Lab’s medium-lift launch vehicle currently in development, targeting payloads up to 13,000 kg to low Earth orbit in reusable configuration (or up to 15,000

Payload to LEO (reusable)	13,000 kg
Payload to LEO (expendable)	15,000 kg
Propellant	Liquid oxygen / liquid methane (methalox)
Engines	Archimedes (first stage: 7 engines; second stage: 1 engine)
Height	~40 m

price on requestdatasheet

Designs, builds, and tests reusable LOX/methane rocket engines and orbital transfer vehicles

Rocket Propulsion Systems (RPS)

RPS Suborbital Launch Vehicle

The RPS Suborbital Launch Vehicle is a single-stage, reusable, liquid-fueled, vertical takeoff rocket designed for suborbital flights for commercial, government, and defense applic

Stages	single-stage, VTVL
Target apogee	50-100 km
Prototype testing	targeted 2026

price on request

Turkish defense company developing missiles, rockets, and space launch systems including sounding rockets and orbital launch vehicle development programs.

Roketsan

Sounding Rocket Systems

Turkish sounding rocket systems for atmospheric research and microgravity experiments — foundational technology for Turkey's planned indigenous orbital launch vehicle program.

Vehicle Type	Suborbital sounding rocket
Propulsion	Solid rocket motor
Applications	Atmospheric research, microgravity experiments, tech demonstration
Program Context	Turkish National Space Program (2021)
Customer	Turkish Space Agency (TUA), research institutions

price on request

Swiss-Swedish space components manufacturer providing satellite structures, thermal control products, payload electronics, and antennas for commercial and institutional programs.

RUAG Space

Ariane 5 / Ariane 6 Structural Components and VESPA Satellite Adapter

Beyond Gravity (formerly RUAG Space) is a Swiss-Swedish space technology company providing structural components, avionics, and satellite dispenser systems for European launchers a

price on request

RUAG Space

Composite Payload Fairings

Composite payload fairings from 0.7 m to 5.4 m diameter, used on Ariane, Vega, Atlas, Vulcan and H3, with a 100% success rate over 400+ launches.

Diameter range	0.7 m to 5.4 m
Construction	Aluminium honeycomb core with carbon fibre reinforced composite cover layers
Manufacturing	Automated industrial process, no autoclave required
Flight record	Over 400 launches, 100% success rate
Launch vehicles	Ariane, Vega, Atlas, Vulcan, H3

price on request

The Shanghai Academy of Spaceflight Technology (SAST) is a major Chinese aerospace research and manufacturing organization founded in 1961, responsible for developing Long March launch vehicles, Fengyun weather satellites, Tianzhou cargo sp

Chinese developer and manufacturer of small solid rockets, weather-modification rocket systems, sounding rockets, guided rockets, and advanced aerospace materials.

Shaanxi Zhongtian Rocket Technology Co., Ltd.

Rocket Overall (Multiple Products)

This page describes a range of rocket products, including weather modification rockets, sounding rockets for atmospheric data collection, air-to-ground rockets, lightning rockets,

WR-98 Rain-enhancement and Hail-suppression Rocket - Characteristics	High nucleus forming rate, rapid nucleation rate, high seeding intensity, large seeding ra
WR-98 Rain-enhancement and Hail-suppression Rocket - Operation advantages	Round-the-clock, all-weather, suitable for all kinds of weather conditions
WR-98 Rain-enhancement and Hail-suppression Rocket - Patents	Obtained a number of patents
WR-98 Rain-enhancement and Hail-suppression Rocket - Usage	Most widely used in weather modification operation in China
WR-98Z Ejectable-flare Rain-enhancement and Hail-suppression Rocket - Seeding method	Advanced ejectable-flare seeding method for high-efficiency three-dimensional cloud seedin

price on request

Shaanxi Zhongtian Rocket Technology Co., Ltd.

Rocket Overall (Product Series)

This page describes a series of rockets developed by the company, including weather modification rockets, sounding rockets for atmospheric data collection, air-to-ground rockets, l

WR-98 Rain-enhancement and Hail-suppression Rocket - Characteristics	High nucleus forming rate, rapid nucleation rate, high seeding intensity, large seeding ra
WR-98 Rain-enhancement and Hail-suppression Rocket - Operation advantages	Round-the-clock, all-weather, suitable for all kinds of weather conditions
WR-98Z Ejectable-flare Rain-enhancement and Hail-suppression Rocket - Characteristics	High nucleus forming rate, rapid nucleation rate, high seeding intensity, large seeding ra
TK-1 Low Altitude Sounding Rocket - Detection altitude range	1000m
TK-2 Sounding Rocket - Detecting range	8km

price on request

Shaanxi Zhongtian Rocket Technology Co., Ltd.

Rocket Overall (WR-98, WR-98Z, TK-1, TK-2, TL-2, Lightning Rocket, TC Series, UAV Airdrops, Serialised Target Rocket, Bo

This page describes a range of rockets including weather modification rockets, sounding rockets for atmospheric data collection, an air-to-ground rocket, a lightning research rocke

price on request

French startup developing a family of reusable small-satellite launch vehicles.

Sirius Space Services

SIRIUS 1

SIRIUS 1 is Sirius Space Services' flagship dedicated small-satellite launch vehicle, a two-stage rocket powered by the company's in-house methalox STAR-1 engine, designed as the f

Payload to SSO 500 km @ 50°	300 kg
Height	34.9 m
Stages	2
Liftoff mass	180 tons
Engine	STAR-1 (methalox, 9 on stage 1, 1 on stage 2)

price on request

India's first private launch company; developing Vikram family of rockets (350–900 kg to LEO); India's first space-tech unicorn (May 2026).

Skyroot Aerospace

Vikram-1

Vikram-1 is Skyroot Aerospace's orbital small-satellite launch vehicle, a four-stage rocket designed to deliver small satellites to low Earth orbit affordably and on demand.

Height	~20 m
Stages	4 (3 solid stages + 1 liquid propulsion upper stage)
Stage 1	Kalam-1000, solid propellant, 1,000 kN thrust
Stage 2	Kalam-250, solid propellant, 250 kN thrust
Stage 3	Kalam-100, solid propellant, 100 kN thrust

price on request

Skyroot Aerospace

Vikram-II Launch Vehicle

India's next-generation small satellite launch vehicle with a cryogenic engine, targeting up to 900 kg to LEO and 600 kg to SSO, launching in 2027.

Payload to LEO	Up to 900 kg
Payload to SSO	Up to 600 kg
Propulsion	Advanced cryogenic engine
Structure	Carbon composite
Launch modes	Dedicated and rideshare

price on request

Skyrora designs, manufactures, and deploys rockets and provides space services for small satellite manufacturers and orbital spacecrafts.

Skyrora

Skylark L

Skylark L is a guided suborbital launch vehicle designed to carry payloads to an apogee altitude of 102 km.

Length	11.65 m
Diameter	0.7 m
Lift-off mass	2,466 kg
Payload mass	50 kg
Propellant	HTP / KEROSENE

price on request

Skyrora

Skylark Micro

Skylark Micro is a suborbital launch vehicle designed for testing electrical systems under g-force, evaluating payload material construction and thermal coatings, and launching sma

Length	3.32 m
Propellant	HTPB
Airframe diameter of the First stage	0.102 M
Thrust of the First stage	1.56 kN
Airframe diameter of the Second stage	0.075 M

price on request

Skyrora

Skylark Nano

Skylark Nano is a suborbital launch vehicle designed for research and data collection, featuring simple pre-launch and launch operations.

Diameter	0.102 M
Propellant	HTPB
Lift-off mass	13.325 KG
Payload mass	UP TO 1 KG
Maximum thrust	1 825 N (182.5 KG)

price on request

Skyrora

Skyrora XL

Skyrora XL is a three-stage orbital launch vehicle designed to deliver payloads of up to 315 kg to orbit.

Length	22.7 m
Diameter	2.2 m
Lift-off mass	55,838 kg
Payload mass	Up to 315 kg
Propellant	HTP / kerosene

price on request

Skyrora

Third Stage

The third stage of the Skyrora XL launch vehicle is a versatile orbital installation vehicle designed to deliver payloads to their chosen orbital inclination.

Length	1.4 M
Diameter	1.9 M
Dry mass	314 KG
Loading mass	590 KG
Propellant	HTP / KEROSENE

price on request

Japanese commercial launch company; KAIROS four-stage solid-propellant small launch vehicle; Kii Spaceport in Wakayama; Canon Electronics, IHI, and Shimizu backed.

Space One — KAIROS

KAIROS

Space One's four-stage solid/liquid commercial small launch vehicle — Japan's first domestically developed private orbital rocket.

Stages	4 (3 solid + 1 liquid)
Payload to SSO	~250 kg
Launch Site	Kii Spaceport, Kushimoto, Wakayama, Japan (private)
First Attempt	March 13, 2024 (anomaly at T+5s)
Operators	Space One Co., Ltd. (Canon Electronics, IHI Aerospace)

price on request

Chinese commercial launch company and developer of the Tianlong rocket family, the first Chinese private firm to reach orbit with a liquid-propellant rocket.

Space Pioneer (Tianbing Technology)

Tianlong-2

Kerosene-liquid oxygen orbital rocket; first Chinese private liquid-propellant vehicle to reach orbit (April 2023).

Propellant	Kerosene / liquid oxygen (kerolox)
Height	32.8 m
Payload to LEO	~2,000 kg
Payload to 500 km SSO	~1,500 kg
Maiden flight	April 2, 2023 (success)

price on request

Space Pioneer (Tianbing Technology)

Tianlong-3

Larger, partially reusable Falcon 9-class rocket in development, targeting ~17,000 kg to LEO.

Propellant	Kerosene / liquid oxygen (kerolox)
Configuration	Two-stage, reusable first stage
Payload to LEO	~17,000 kg
Payload to 500 km SSO	~14,000 kg
Class	Falcon 9-class

price on request

SpaceForest designs and manufactures synthetic aperture radars, advanced electronics, microwave filters, and suborbital and supersonic rockets, offering flight services and technology testing for vari

SpaceForest

Perun Small Orbital Launch Vehicle

SpaceForest's Perun — Poland's planned first orbital launch vehicle, using hybrid propulsion to target 50–100 kg to LEO from European spaceports.

Vehicle Type	Small orbital launch vehicle (hybrid propulsion)
Payload to LEO	50–100 kg (target)
Heritage	SRT-2 sounding rocket + Bursztyn hybrid engine (>100 km achieved)
Propulsion	Hybrid (liquid oxidizer / solid fuel grain)
Launch Site	European spaceport (SaxaVord, Andøya candidates)

price on request

Fully-reusable launch services to LEO, GTO, GEO, TLI and beyond — Falcon 9, Falcon Heavy, Starship.

SpaceX

Falcon 9

Partially reusable two-stage orbital rocket and the world's first commercially successful reusable orbital launch vehicle.

Payload to LEO	22,800 kg
Payload to GTO	8,300 kg
Payload to GEO (direct)	3,500 kg
First stage engines	9× Merlin 1D (sea-level)
Second stage engine	1× Merlin 1D Vacuum

price on requestdatasheet

SpaceX

Falcon Heavy

SpaceX's heavy-lift partially reusable launch vehicle combining three Falcon 9 first-stage cores.

Payload to LEO	63,800 kg (expended)
Payload to GTO	26,700 kg (expended) / 16,800 kg (reusable)
Total first-stage engines	27× Merlin 1D
Height	70 m
Liftoff thrust	22,819 kN

price on requestdatasheet

SpaceX

Starship

SpaceX's fully reusable super-heavy-lift launch system designed to carry humans and cargo to the Moon, Mars, and beyond.

Payload to LEO (reusable)	>100,000 kg
Payload to LEO (expendable)	~150,000 kg
Super Heavy engines	33× Raptor 2 (methane/LOX)
Starship engines	6× Raptor (3 sea-level + 3 vacuum)
Total liftoff thrust	>74,000 kN

price on request

SpinLaunch develops a kinetic (non-combustion) launch system that uses a rotating vacuum-sealed accelerator to hurl launch vehicles toward space, and operates Meridian Space, a low-cost LEO satellite communications constellation business.

SpinLaunch

SpinLaunch Orbital Launch System

A kinetic (non-combustion) orbital launch system that uses a rotating carbon-fiber arm inside a 100-meter vacuum chamber to accelerate a launch vehicle to 8,000 kph before a small

Launch method	Kinetic (rotating carbon-fiber arm in vacuum chamber)
Vacuum chamber diameter	100 meters
Release velocity	Up to 8,000 kph
Fuel/structure reduction vs. typical rocket	Up to 70%
Orbital insertion	Small propulsive upper stage completes ascent to orbit

price on request

Stoke Space designs and manufactures 100% reusable Nova rockets and their components for affordable access to and from orbit.

Stoke Space

Nova

Stoke Space's fully reusable small launch vehicle with a hydrogen-powered upper stage capable of propulsive reentry, targeting 2025–2026 first flight.

Payload to LEO	~2,000 kg (reusable)
Propellants	LOX/LH2 (both stages)
Upper Stage	Annular aerospike with rotating heat shield — fully propulsively reusable
Test Site	Moses Lake, Washington
Status	Development, first flight targeting 2025–2026

price on request

Dutch manufacturer of solid-propellant suborbital sounding rockets and hypersonic test vehicles

T-Minus Engineering

T-Minus DART

The T-Minus DART is a low-cost, rapidly deployable sounding rocket system designed for probing the upper atmosphere (50-120 km altitude) and launching small scientific payloads abo

Booster Motor Diameter	0.118 [m] (Viper IIA compatible)
Booster Motor Length	2.3 [m]
Booster Motor Burn time	5 [s]
Booster Motor Average thrust	8 [kN]
Booster Motor Propellant mass	22 [kg]

price on requestdatasheet

TiSPACE (Taiwan Innovative Space) is a private Taiwanese company specializing in hybrid-propulsion space launch vehicles and dedicated small-satellite launch services.

TiSPACE (Taiwan Innovative Space)

Hapith I

TiSPACE's first-generation hybrid-propulsion launch vehicle, flight-tested from Australia under the company's first international launch permit.

Propulsion Type	Non-explosive hybrid rocket propulsion
First Launch Permit	Granted by the Australian Government, 9 August 2021

price on request

TiSPACE (Taiwan Innovative Space)

Hapith V

Three-stage orbital launch vehicle using TiSPACE's non-explosive hybrid rocket propulsion technology, designed for dedicated launch of micro and small satellites to LEO and SSO.

Max. LEO Payload Mass	390 kg
Max. SSO Payload Mass	350 kg
Target Altitude	600-700 km
Height	20 m
Diameter	2.2 m

price on request

Heavy-lift national-security launch services — Vulcan Centaur, Atlas V.

United Launch Alliance (ULA)

Atlas V

Atlas V is United Launch Alliance’s proven medium-to-heavy launch vehicle with a 100% mission success record across over 100 flights. Powered by a single RD-180 engine on its

First Stage Engine	1× RD-180 (LOX/RP-1)
Upper Stage	Centaur, 1 or 2× RL-10
Payload to LEO	up to 18,850 kg (HLV config)
Payload to GTO	up to 8,900 kg
Mission Success Rate	100% (100+ flights)

price on requestdatasheet

United Launch Alliance (ULA)

Vulcan Centaur

Vulcan Centaur is United Launch Alliance’s (ULA) next-generation rocket designed to replace both the Atlas V and Delta IV Heavy launch vehicles. The two-stage rocket uses two

First Stage Engines	2× Blue Origin BE-4 (LOX/LNG)
Upper Stage	Centaur V, 2× RL-10
Payload to LEO	up to 27,200 kg (VC6 config)
Payload to GTO	up to 13,080 kg (VC6 config)
Fairing Diameter	5.4 m

price on requestdatasheet

US suborbital launch provider operating the SpaceLoft XL sounding rocket from Spaceport America in New Mexico for microgravity research and technology demonstration.

UP Aerospace

SpaceLoft XL

Flight-proven solid-fuel suborbital sounding rocket providing low-cost microgravity and hypersonic test flights from Spaceport America.

Payload capacity	36 kg (79 lb)
Altitude	120–225 km
Stages	1 (solid-fuel)
Microgravity duration	Up to 5 minutes
First flight	25 September 2006

price on request

UP Aerospace

Spyder Sub-Orbital Vehicle

High-performance single-stage suborbital rocket capable of Mach 10+ speeds and 400 km altitude, developed with NASA support.

Diameter	17.25 in
Max speed	Mach 10+
Max altitude	400 km
Stages	1
First flight	June 2025

price on request

Vaya Space develops and manufactures advanced hybrid propulsion systems for defense and space applications, utilizing its patented Vortex-Hybrid engine.

Vaya Space

Dauntless

Two-stage small-satellite launch vehicle powered by Vaya Space's vortex-hybrid STAR-3D engines.

Height	35 m (~115 ft)
Stage 1 diameter	2.5 m (~8 ft)
Stage 2 diameter	2.15 m (~7 ft)
Fairing diameter	2.15 m (~7 ft)
Stages	2

price on request

Yuzhnoye State Design Office (KB Pivdenne) is Ukraine's premier rocket and space engineering organization, providing full-cycle development of launch vehicles, spacecraft, and propulsion systems. Founded in 1954 and headquartered in Dnipro,

Yuzhnoye Design Bureau

Antares

The Antares is a medium-lift class two-stage launch vehicle developed through collaboration between Orbital Sciences Corporation (now Northrop Grumman) and Ukraine’s Yuzhnoye

Vehicle Class	Medium-lift
Number of Stages	2
Height	42,500 mm
Body Diameter	3,900 mm
Gross Mass (without payload)	330 t

price on request

Yuzhnoye Design Bureau

Cyclone-1

The Cyclone-1 is a lightweight three-stage liquid-propellant launch vehicle developed by Yuzhnoye SDO for deploying payloads into low Earth orbits, including sun-synchronous orbits

Vehicle Class	Lightweight
Number of Stages	3
Height	30,000 mm
Body Diameter	2,250 mm
Fairing Diameter	2,250 mm

price on request

Yuzhnoye Design Bureau

Cyclone-4M

The Cyclone-4M is a two-stage medium-lift class launch vehicle developed by Yuzhnoye SDO for deploying spacecraft into low, medium, and high near-Earth orbits, including sun-synchr

Vehicle Class	Medium-lift
Number of Stages	2
Height	39,000 mm
Body Diameter	3,900 mm
Fairing Diameter	4,000 mm

price on request

Yuzhnoye Design Bureau

Cyclone-5

The Cyclone-5 is a three-stage medium-lift class monoblock launch vehicle developed by Yuzhnoye SDO for placing spacecraft into low, medium, and high Earth orbits including geostat

Vehicle Class	Medium-lift
Number of Stages	3
Height	51,000 mm
Body Diameter	3,900 mm
Fairing Diameter	4,000 mm

price on request

Yuzhnoye Design Bureau

Heavy Lunar Lander

The Heavy Lunar Lander is a large-payload lunar surface delivery vehicle developed by Yuzhnoye SDO, designed to deliver up to 10 tonnes of useful payload to the lunar surface. This

Payload Capacity to Lunar Surface	Up to 10 tonnes
Primary Applications	Lunar base modules, manned vehicles

price on request

Yuzhnoye Design Bureau

Mayak-M-3.9

The Mayak-M-3.9 is a two-stage heavy-lift class launch vehicle developed by Yuzhnoye SDO, utilizing RD815 engines on the first stage and technologies derived from the proven Zenit,

Vehicle Class	Heavy-lift
Number of Stages	2
Height	65,000 mm
Body Diameter	3,900 mm
Fairing Diameter	4,200 mm

price on request

Yuzhnoye Design Bureau

Mayak-SH-3

The Mayak-SH-3 is a super heavy-lift class two-stage launch vehicle developed by Yuzhnoye SDO, capable of placing 59.3 tonnes into low Earth orbit and 18.7 tonnes on a lunar trajec

Vehicle Class	Super heavy-lift
Number of Stages	2
Height	75,000 mm
Body Diameter	3,900 mm
Fairing Diameter	5,100 mm

price on request

Yuzhnoye Design Bureau

Mayak-SH-5

The Mayak-SH-5 is a super heavy-lift class two-stage launch vehicle developed by Yuzhnoye SDO, capable of placing 93.2 tonnes into low Earth orbit and 30.5 tonnes on a lunar trajec

Vehicle Class	Super heavy-lift
Number of Stages	2
Height	80,000 mm
Body Diameter	3,900 mm
Fairing Diameter	6,200 mm

price on request

Yuzhnoye Design Bureau

Mayak-SH-7

The Mayak-SH-7 is the largest variant in Yuzhnoye SDO’s Mayak super heavy-lift launch vehicle family, capable of delivering 133 tonnes to low Earth orbit and 40 tonnes on a l

Vehicle Class	Super heavy-lift
Number of Stages	2
Height	79,900 mm
Body Diameter	3,900 mm
Fairing Diameter	6,200 mm

price on request

Yuzhnoye Design Bureau

SLS Mobile Basing

The Space Launch System (SLS) Mobile Basing is a road-mobile launch solution developed by Yuzhnoye SDO for launching meteorological rockets to altitudes up to 100 km. The mobile la

Application	Meteorological rockets to 100 km altitude
Vehicle Configuration	6x2 or 6x4 wheeled
Diesel Engine Power	250 to 400 kW
Emission Standard	Euro 5
Cruising Range	900 km

price on request