Space Hardware Marketplace

Mercury Series CubeSat Dispensers

• Mercury-33U lightweight dispenser, rail-type CubeSats, qualified to NASA GEVS levels, flight-proven
• Mercury-66U lightweight dispenser, rail-type CubeSats, qualified to NASA GEVS levels, flight-proven
• Mercury-6T6U tab-based dispenser, tab-type CubeSats, over 50% reduction in gRMS environment transmission, flight-proven

Maverick Space Systems' flagship hardware line: a family of lightweight, flight-proven CubeSat dispensers (Mercury-3, -6, -6T, -12, -12T,…

Hybrid Propulsion System (HIS)

• Fuel typeHigh-performance solid fuel
• Average thrust650 N
• Specific impulse290 s

A domestically-developed hybrid rocket propulsion system by DELTAV Space Technologies, designed for Turkey's AYAP-1 lunar hard-landing mission and…

Bishop Airlock

• Mass1,059 kg
• Height1.80 m
• Diameter2.014 m

Bishop is the first permanent commercial airlock module on the International Space Station, built and operated by Nanoracks…

SlingShot

• Deployment capacityUp to 72U of CubeSats per Cygnus mission
• Maximum single payload size12U CubeSat
• Compatible CubeSat formats1U, 2U, 3U Rail, 6U Rail, 6U Tab, 12U Rail, 12U Tab

SlingShot is SEOPS' flagship CubeSat/small-satellite deployer that rides on Northrop Grumman's Cygnus spacecraft, deploying payloads at an altitude…

Antares 330

• StagesTwo-stage: liquid-fueled first stage + solid-fueled second stage
• First stage engines7x Firefly Aerospace Miranda engines (RP-1/LOX)
• First stage thrust~7,200 kN combined

Antares 330 is Northrop Grumman's next-generation, two-stage expendable rocket designed to launch Cygnus cargo spacecraft to the ISS,…

New Glenn

• Height~98 m
• Diameter7 m
• Stages2 (reusable first stage, expendable second stage)

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

Vulcan Centaur

• First Stage Engines2× Blue Origin BE-4 (LOX/LNG)
• Upper StageCentaur V, 2× RL-10
• Payload to LEOup to 27,200 kg (VC6 config)

ULA's next-generation medium-to-heavy launch vehicle powered by two BE-4 engines, replacing Atlas V for US national security and…

Ariane 6

• Ariane 62 payload to GTO~3,500 kg
• Ariane 64 payload to GTO~5,000 kg
• Ariane 62 payload to LEO~10,300 kg

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

Electron

• Height18 m
• Diameter1.2 m
• Mass13.0 t

Electron is Rocket Lab's operational two-stage (optionally three-stage) small-satellite launch vehicle, built from carbon composite and powered by…

Falcon 9

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

Perun Small Orbital Launch Vehicle

• Vehicle TypeSmall orbital launch vehicle (hybrid propulsion)
• Payload to LEO50–100 kg (target)
• HeritageSRT-2 sounding rocket + Bursztyn hybrid engine (>100 km achieved)

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

Nyx

• ConfigurationConical reentry capsule + cylindrical service module
• Diameter (Nyx Earth)4 m
• Height (Nyx Earth)7 m

Nyx is a reusable European reentry capsule developed by The Exploration Company to deliver cargo to and from…

Maia

• Height50 m
• Diameter3.5 m
• Stages2 stages (plus optional Colibri third stage/kick stage)

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

ZERO

• Height32 m
• Diameter1.7 m
• Mass71 t

ZERO is a two-stage, small orbital launch vehicle being developed by Japan's Interstellar Technologies to carry up to…

Orbital Baguette One

• Height~16 m
• PropulsionHybrid rocket engine ('Terminator'): solid HDPE fuel grain + liquid oxidizer, helium-pressurized, turbopump-free
• Engine thrust (demonstrator)~100 kN

OB-1 is HyPrSpace's orbital micro-launcher under development in France, using a turbopump-free hybrid rocket engine to deliver up…

Zephyr

• Stages2
• PropellantsLOX/Methane (both stages)
• EngineNavier (in-house, additive manufactured)

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

Daytona

• Payload to LEO~450 kg
• PropellantsLOX/Kerosene
• HQTucson, Arizona, USA

Phantom Space's small orbital launch vehicle targeting 450 kg to LEO using liquid propellants with a focus on…

YAM Platform

• Product typeRideshare hosted-payload smallsat platform / space infrastructure-as-a-service
• Bus optionsBlue Canyon Technologies MicroSat/ESPAsat (YAM-2); LeoStella bus (YAM-3, YAM-5, YAM-6); Airbus Arrow 150 'Longbow' (YAM-8 and later)
• YAM-2 mass~80 kg

Loft Orbital's YAM (Yet Another Mission) is a rideshare hosted-payload satellite platform offering infrastructure-as-a-service in orbit, letting customers…