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SAE technical paper series, Volume 941197.
A functional model for the transfer of aerospace technology to commercial industry is presented. Honeycomb damping seals are presented as an example technology... 
Rocket engines
eJournal
SAE technical paper series, Volume 929200.
A two Tesla test facility was designed, built, and operated to investigate the performance of magnetohydrodynamic (MHD) seawater thrusters. The results of this... 
Rocket engines
eJournal
SAE technical paper series, Volume 730944.
A new rocket engine concept that is presently being evaluated offers significant performance, cost, and configurational advantages. The Linear Rocket Engine... 
Rocket engines
eJournal
SAE technical paper series, Volume 2007-01-3860.
Since the advent of the helicopter, aviation designers have struggled to develop a practical vertical lift propulsion concept that could combine the vertical... 
Rocket engines
eJournal
SAE technical paper series, Volume 830116.
We analyze a number of existing and proposed automotive propulsion systems and compare their specific energy and specific peak power in terms of mechanical... 
Rocket engines
eJournal
SAE technical paper series, Volume 881029.
After a hiatus of nearly 20 years, NASA is once again actively examining manned Mars missions. As part of this activity, a very recent engineering study has... 
Rocket engines
eJournal
SAE technical paper series, Volume 730941.
Apollo 17 ended the most successful application of rocket propulsion systems in man's history. A total of 23 developmental and manned operational flights were... 
Rocket engines
eJournal
SAE technical paper series, Volume 740831.
The aerodynamic design of the F-12 engine air inlet is discussed following development from its inception to the present configuration. A description of the... 
Rocket engines
eJournal
SAE technical paper series, Volume 750629.
Since 1972 NASA has pursued a program aimed at advancing the technology and establishing a data base appropriate for the possible future development of... 
Rocket engines
eJournal
SAE technical paper series, Volume 710765.
The Algol III is a new high-performance solid rocket motor developed for use as the first stage of the NASA SCOUT-D and -E launch vehicles. The motor delivers... 
Rocket engines
eJournal
SAE technical paper series, Volume 720839.
The requirements of the Space Shuttle Bipropellant RCS Engine Technology contract and the scheduled contract effort are presented hereinches The requirements... 
Rocket engines
eJournal
SAE technical paper series, Volume 941710.
Because of the rapid progress in the electronics field during the last few years coupled with the ever increasing use of computer based systems on board ships,... 
Rocket engines
eJournal
SAE technical paper series, Volume 710766.
Light weight solid propellant motors which supply high thrusts (andgt;500 lbf) for durations on the order 0.010 sec. (referred to as impulsive thrusters)... 
Rocket engines
eJournal
SAE technical paper series, Volume 929199.
Loss mechanisms affecting the performance of an MHD seawater thruster system have been identified and discussed. Among those losses are the jet and nozzle... 
Rocket engines
eJournal
SAE technical paper series, Volume 901044.
The Earth-to-Orbit (ETO) Propulsion Program was initiated in 1988 as a major element of NASA's Civil Space Technology Initiative (CSTI), a set of some ten... 
Rocket engines
eJournal
SAE technical paper series, Volume 831494.
A medium speed V/STOL aircraft has been configured using a tandem fan propulsion system concept. Each tandem fan nacelle has two unique inlets and nozzles.... 
Rocket engines
eJournal
SAE technical paper series, Volume 700819.
The design of the propulsion control system for the Supersonic Transport (SST) is a culmination of three years of design trade studies. An analysis was made of... 
Rocket engines
eJournal
SAE technical paper series, Volume 962274.
Analysis and testing are used to show the feasibility of an innovative shaft driven lift fan propulsion system for supersonic STOVL aircraft. Dual cycle... 
Rocket engines
eJournal
SAE technical paper series, Volume 942122.
The technical thermodynamics solution of rocket engine cycle optimization is introduced here. The traditional approximations of thrust production process are... 
Rocket engines
eJournal
SAE technical paper series, Volume 751085.
The concerns for limited availability of petroleum based fuels and the upward cost spiral of oil has resulted in great interest in fuel consumption in the... 
Rocket engines
eJournal
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