Propulsion — Space Hardware Marketplace

GATE Jetpack Propulsion Module

• Total impulse (S/M/L)36,000 / 80,000 / 140,000 Ns
• Thrust (S)4x [1-6N]
• Thrust (M/L)4x [20N]

Plug-and-play chemical propulsion module for ESPA-class satellites — 3 sizes (S/M/L), 36,000-140,000 Ns total impulse, orbit transfer and…

Pulsed Plasma Rocket (PPR)

NASA NIAC-funded nuclear pulsed-plasma propulsion concept aiming to cut crewed Mars transit time to about two months —…

ATHENA Electric Propulsion

• TechnologyElectrospray propulsion
• Model variantsPICO, NANO, MICRO (upcoming)
• ApplicationsOrbit correction, life extension, deorbiting, constellation deployment, collision avoidance

World's most compact on-board electric propulsion systems based on electrospray technology — available in PICO, NANO, and upcoming…

GITA — Green Impulse Transmitter

• Propellant typeRefuellable, easy-to-source
• PerformanceHigh thrust, higher impulse
• ResponseInstant response capabilities

Eco-friendly propulsion system powering in-orbit servicing vehicles — refuellable, easy-to-source propellants, high thrust and instant response capabilities.

Cold Gas Propulsion Module

• Thrust1-13 mN
• Impulse>420 Ns
• Dimensions1U (100 x 100 x 110 mm)

Low-power, plug-and-play cold gas module for CubeSats 2U+ — 1-13mN thrust, >420 Ns impulse, qualified per SpaceX Falcon…

HALO-100X Electrospray Propulsion Module

• Form factor1U
• Weight1.2 kg
• Power40-50 W

Plug-and-play 1U electrospray electric propulsion module — inert non-toxic propellant, >5000s Isp, configurable high-thrust boost or high-ISP endurance…

Air-Breathing Electric Propulsion (ABEP) Thruster

• Satellite platform lifetime>7 years
• Operating altitudeCan extend below 200 km
• PropellantNone required — ingests atmospheric gas

Electric thruster ingesting residual atmospheric particles at Very Low Earth Orbit and converting them to plasma for continuous…

DARUMA Micro Hybrid Propulsion Unit

• Wet mass30 kg
• Performance (10kg payload)Accelerates to 1,100 m/s
• Performance (100kg payload)Accelerates to 400 m/s

Modular hybrid propulsion unit using solid HDPE fuel and N2O oxidizer for last-mile orbital maneuvers of small satellites…

BOOSTER Green Propulsion System

• Thrust classes1N (0.49-1.42N), 5N (2.62-7.62N), 20N (10.5-30.5N), 200N (138-241N)
• Specific impulse273-303 s (varies by class)
• PropellantsN2O + C2H6

Modular green chemical propulsion system family for small satellites — thrust classes from 1N to 200N, N2O/C2H6 propellants,…

Solar Sails (Space Propulsion)

• Ground-deployed sail sizes83 sq m and 318 sq m
• Sunjammer solar sail1200 sq m total (300 sq m quadrant deployed)
• Deployment mechanism4 independently-controlled sub-Tg conically-deployed composite booms

Large deployable solar sails using proprietary stripe net architecture for propellant-free deep-space propulsion — 300 sq m quadrant…

Vyom 2U Monopropellant Propulsion System

• Satellite weight5U to 24U+ satellites
• Thrust1.1 N
• Specific impulse~250 s (BOL)

Flight-proven 1N monopropellant green propulsion system for 5U-24U+ satellites — flew aboard ISRO's PSLV-C60 POEM-4, 700+ seconds cumulative…

Sharanga Micro-Propulsion System

• Satellite weight3U to 10U+ satellites
• Nominal thrust1 to 10 mN
• Specific impulse~150 s (BOL)

Self-pressurizing micro-propulsion system with 1-10 mN thrust for CubeSats up to 50kg — non-toxic HTP monopropellant, flight-tested at…

I-Booster Green Propulsion System

• Satellite weight100-500 kg
• Nominal thrust0.5 N, 1 N
• Specific impulse~250 s (BOL)

Green chemical propulsion system with 4x1N thrusters for 100-500kg satellites — hydrazine-free alternative delivered to India's DRDO for…

GP-LAM Liquid Apogee Module

• Spacecraft typeOTVs, launch vehicle upper stage, GEO stationary satellite
• Nominal thrust300 N (BOL)
• Specific impulse250 s (BOL)

300N modular green propulsion Liquid Apogee Module for launch vehicle upper stages, OTVs, and GEO spacecraft — multi-restart…

Hatchet Rocket Engine

• Thrust750 lbf
• PropellantsLiquid Oxygen / Isopropyl Alcohol
• Flight heritage220+ successful flights, 15,000+ seconds of operation

750 lbf thrust engine used on the Xombie vehicle — 220+ successful flights, 15,000+ seconds of operation heritage,…

Tachi Rocket Engine

• Thrust6,000 lbf
• PropellantLiquid Oxygen / Liquid Methane
• Manufacturing methodPermiAM (patent-pending additive manufacturing)

6,000 lbf reusable liquid-propellant rocket engine built with PermiAM additive manufacturing — deep throttling, low mass, expandable to…

Broadsword Rocket Engine

• Thrust25,000 lbf
• CycleDual expander
• PropellantsLiquid Oxygen / Methane

25,000 lbf dual expander cycle engine developed through DARPA XS-1 and NASA Tipping Point programs — additively manufactured…

Scimitar Rocket Engine

• Thrust1,200 lbf
• PropellantsLiquid Oxygen / Isopropyl Alcohol
• Flight heritage100+ successful flights, 35,000+ seconds of operation

1,200 lbf thrust main engine currently powering the Xodiac vehicle — 100+ successful flights, 35,000+ seconds of total…