Add to ORKGThis slide presentation reviews the JSC Energy Systems Divisions work in propulsion. Specific work in LO2/CH4 propulsion, cryogenic propulsion, low thrust propulsion for Free Flyer, robotic and Extra Vehicular Activities, and work on the Morpheus terrestrial free flyer test bed is reviewed. The back-up slides contain a chart with comparisons of LO2/LCH4 with other propellants, and reviewing the advantages especially for spacecraft propulsion
Liquid oxygen (LOX)/hydrocarbon propulsion concepts for a "second generation' orbiter auxiliary prop...
The test results of small LOX/LH2 engines for two propulsion systems, a pump fed system and a pressu...
NASA is pursuing non-toxic propellant technologies applicable to RLV and Space Shuttle orbital maneu...
The National Aeronautics and Space Administration (NASA) has identified liquid oxygen (LO2)/liquid m...
The proposed paper will cover ongoing work at the National Aeronautics and Space Administration (NAS...
The National Aeronautics & Space Administration (NASA) has identified Liquid Oxygen (LOX)/Liquid Met...
The topics presented are covered in viewgraph form. The programmatic objective is to provide the tec...
Initiatives have emerged with the goal of sending humans to other places in our solar system. New te...
Initiatives have emerged with the goal of sending humans to other places in our solar system. New te...
Liquid oxygen (LOX) and liquid methane (LCH4) are a propellant combination viewed as a potential ena...
Lander Tech is three separate but synergistic efforts: Lunar CATALYST (Lunar Cargo Transportation an...
Liquid oxygen (LOX) and liquid methane (LCH4) are a propellant combination viewed as a potential ena...
NASA's Vision for Exploration requires a safe, reliable, affordable upper stage engine to power the ...
The National Aeronautics & Space Administration (NASA) has identified Liquid Oxygen (LOX)/Liquid Met...
Topics addressed are: (1) cryogenic tankage; (2) launch vehicle TPS/insulation; (3) durable passive ...
Liquid oxygen (LOX)/hydrocarbon propulsion concepts for a "second generation' orbiter auxiliary prop...
The test results of small LOX/LH2 engines for two propulsion systems, a pump fed system and a pressu...
NASA is pursuing non-toxic propellant technologies applicable to RLV and Space Shuttle orbital maneu...
The National Aeronautics and Space Administration (NASA) has identified liquid oxygen (LO2)/liquid m...
The proposed paper will cover ongoing work at the National Aeronautics and Space Administration (NAS...
The National Aeronautics & Space Administration (NASA) has identified Liquid Oxygen (LOX)/Liquid Met...
The topics presented are covered in viewgraph form. The programmatic objective is to provide the tec...
Initiatives have emerged with the goal of sending humans to other places in our solar system. New te...
Initiatives have emerged with the goal of sending humans to other places in our solar system. New te...
Liquid oxygen (LOX) and liquid methane (LCH4) are a propellant combination viewed as a potential ena...
Lander Tech is three separate but synergistic efforts: Lunar CATALYST (Lunar Cargo Transportation an...
Liquid oxygen (LOX) and liquid methane (LCH4) are a propellant combination viewed as a potential ena...
NASA's Vision for Exploration requires a safe, reliable, affordable upper stage engine to power the ...
The National Aeronautics & Space Administration (NASA) has identified Liquid Oxygen (LOX)/Liquid Met...
Topics addressed are: (1) cryogenic tankage; (2) launch vehicle TPS/insulation; (3) durable passive ...
Liquid oxygen (LOX)/hydrocarbon propulsion concepts for a "second generation' orbiter auxiliary prop...
The test results of small LOX/LH2 engines for two propulsion systems, a pump fed system and a pressu...
NASA is pursuing non-toxic propellant technologies applicable to RLV and Space Shuttle orbital maneu...