Propulsion
Building innovative solutions to power human exploration
Our expertise in design, analysis, systems engineering, integration, manufacturing, and test provides full-spectrum support for launch vehicles, missile systems, and spacecraft.
Rocket Propellants
- Liquid Oxygen, Nitrous Oxide, and Hydrogen Peroxide
 - Kerosene (RP-1), Propane, Ethane, Methane, Hydrogen
 - Hydroxylammonium nitrate (HAN) (AF-315E) and hydrazine
 - Solid and Hybrid rocket motors
 
Testing
- Propulsion testing: up to 50,000-lbf thrust-class engines and stages, cryogenic propellants, storable propellants, in-house vacuum propulsion testing
 - Mechanical testing: pneumatic, cryogenic, and hydraulic systems, structural development and qualification, proof and burst
 - Environmental testing: vibration, temperature cycling, thermal shock, and vacuum
 
RCS Thruster Case Study
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- GOX/GCH4 Propellant
 - Radiatively Cooled Thrust Chamber & Nozzle
 - Additively Manufactured Injector
 - Two Thrust Modes
	
- Nominal Mode for General Maneuvers
 - Low Mode for Fine Control
 
 
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- Nominal Thrust: 890 N (200 lbf)
 - Low Thrust:110 N (25 lbf)
 - ISP: 345 sec
 - O/F Ratio: 3.0
 - Minimum Impulse Bit: 2.75 N-s
 - Design Steady State Duration: >100 sec
 - Design Cycle Life: >100,000 Pulses