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SAE technical paper series, Volume 800295.
Toxicity and flammability hazards of gas generants and exhaust products therefrom are reviewed in comparison to other chemicals commonly used in automobiles.... 
Propellants | Passive restraint systems
eJournal
SAE technical paper series, Volume 2004-01-2313.
Space transportation today is undertaken nearly entirely using vehicles launched from Earth in which all elements of a mission are integrated on Earth.... 
Propellants | Spacecraft | Environment
eJournal
SAE technical paper series, Volume 931451.
This paper describes air breathing reusable space launch vehicle concepts intended to provide very rapid response launch of 10,000 lb polar orbit payloads (or... 
Launch vehicles | Liquid propellants
eJournal
SAE technical paper series, Volume 700796.
Savings of 50 percent can be achieved in ablative nozzles for 260-inches-dia solid rocket motors using present state-of-the-art materials. An optimum nozzle... 
Liquid propellants | Rocket engines
eJournal
SAE technical paper series, Volume 770413.
A theoretical model for predicting the evaporation process of liquid fuel sprays in both diesel and Place of publication not identified stratified charge... 
Liquid propellants | Fuel injection
eJournal
SAE technical paper series, Volume 841526.
A large number of spacecraft scheduled to be launched in the 1980's and 1990's will utilize bipropellant attitude control thrusters. Contaminants generated... 
Propellants | Rocket engines
eJournal
SAE technical paper series, Volume 951733.
Recent concepts for returning sample material from Mars have identified many low-cost approaches. The intention of this study is to create an even playing... 
Propellants | Rocket engines
eJournal
SAE technical paper series, Volume 820841.
Storage of cryogenic fluids in space for long periods is being considered in some mission plans. Weight penalty due to fluid vent loss can be high when lengthy... 
Liquid propellants | Hydrogen fuel
eJournal
SAE technical paper series, Volume 2000-01-2238.
Chemical processing of the dusty, low-pressure Martian atmosphere for production of propellants and other consumables will require conditioning and compression... 
Propellants | Carbon dioxide
eJournal
SAE technical paper series, Volume 2005-01-3412.
Limiting factors in air and space propulsion systems affect both design and operation of the engines and the energy derived from a fuel source. Translation of... 
Propellants | Test procedures | Engines
eJournal
SAE technical paper series, Volume 941166.
Two concepts of rocket based combined cycle for single stage rocket are examined. Concept of SSR power plant consisted of liquid rocket engine and liquid air... 
Liquid propellants | Rocket engines
eJournal
SAE technical paper series, Volume 931437.
The B-2 facility is designed to hot fire rocket engines or upper stage launch vehicles with up to 890,000 N thrust, after environmental conditioning of the... 
Propellants | Rocket engines
eJournal
SAE technical paper series, Volume 2004-01-2316.
The goal of this project is the development and characterization of synthetic membranes for the separation and purification of CO2 from the Martian atmosphere... 
Propellants | Carbon dioxide | Synthetic fuels
eJournal
SAE technical paper series, Volume 1999-01-0884
The development of any sealing product invariably involves some form of physical leakage testing, and although this evaluates the performance of the product,... 
Seals and gaskets | Liquid propellants
eJournal
SAE technical paper series, Volume 700800.
Air Force weapons systems require long-term maintenance-free storage, preferably under uncontrolled environmental conditions. Liquid propulsion system... 
Liquefied petroleum gas | Liquid propellants
eJournal
SAE technical paper series, Volume 2005-01-3413.
Spacecraft designs incorporating a propulsion system powered by a more efficient fuel would greatly reduce the oxidizer to payload ratio. This could be... 
Scramjet engines | Propellants | Rocket engines
eJournal
SAE technical paper series, Volume 911555.
A successful thermal storage system, useful in the 115 K to 120 K temperature range, has been designed and demonstrated in a typical IR sensor satellite... 
Spacecraft | Solid propellants | Thermal management
eJournal
SAE technical paper series, Volume 1999-01-0883
The reliability of a valve stem seal (VSS) is directly related to its ability to deliver the correct rate of lubrication. Too little lubrication may result in... 
Seals and gaskets | Liquid propellants
eJournal
SAE technical paper series, Volume 931446.
The Phillips Laboratory has extensive rocket propulsion facilities at Edwards Air Force Base, California. These facilities range from small scale cells capable... 
Propellants | Test facilities | Rocket engines
eJournal
SAE technical paper series, Volume 900037.
The Rotary Engine is ideally suited to ducted fan propulsion systems. The obvious features of high power density and low vibration are complemented by the... 
Propellants | Hybrid engines | Rotary engines
eJournal
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