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SAE technical paper series, Volume 921043.
This technical paper discusses the evolution of turbopumps designed for U.S. rocket engines, starting with the Thor, Jupiter, and Atlas missiles, which were developed in the 1950s... 
Computational fluid dynamics | Liquefied petroleum gas | Liquid propellants | Rocket engines
eJournal
SAE technical paper series, Volume 861813.
This paper discusses several LOX/Hydrocarbon booster engines that are being considered for future launch vehicles... 
Methane | Launch vehicles | Corrosion | Liquid propellants | Coolants | Rocket engines | Hydrogen fuel | Combustion chambers
eJournal
SAE technical paper series, Volume 975523.
.... However, flight testing continues to play an integral role in the maturation of fighter engines... 
Flight tests | Rocket engines
eJournal
SAE technical paper series, Volume 720806.
The orbit maneuvering engines provide the propulsive thrust to increase or decrease the velocity of the space shuttle orbiter while in earth orbit... 
Spacecraft | Rocket engines
eJournal
SAE technical paper series, Volume 880932.
... engines with some consideratons on questions raised by the vehicule / engine system integration... 
Scramjet engines | Launch vehicles | Rocket engines
eJournal
SAE technical paper series, Volume 921007.
An extensive study of liquid propellant rocket engine test and flight history data has produced methods for advanced health monitoring currently under development for application to the Advanced... 
Hybrid engines | Sensors and Actuators | Wear | Fatigue | Rocket engines | Vehicle performance | Hardware
eJournal
SAE technical paper series, Volume 941698.
In marine propulsion systems with direct-coupled two-stroke large diesel engines, the angular position of the propeller with respect to the crankshaft remains unchanged during the whole operation of the engine... 
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 included an engine concept scalable... 
Rocket engines
eJournal
SAE technical paper series, Volume 921031.
...” for technology development to enable enhanced engine performance with increased reliability, durability and maintainability... 
Hybrid engines | Rocket engines
eJournal
SAE technical paper series, Volume 810455.
The NASA Lewis Research Center (LeRC) as Project Manager of the Department of Energy's Automotive Heat Engine Program, is developing advanced gas turbine and Sterling engines for automobiles... 
Gas turbines | Stirling engines | Solar rocket engines
eJournal
SAE technical paper series, Volume 900993.
...) engines designed for horizontal take-off and landing Single-Stage-to-Orbit (SSTO) vehicles acceleration up to Mach 6... 
Hybrid engines | Rocket engines | Vehicle performance
eJournal
SAE technical paper series, Volume 831496.
...) fighter/attack aircraft has been developed. The concept comprises a variable cycle engine, combining the advantages of a vectored thrust turbofan for takeoff, landing, and subsonic flight with those of a mixed augmented turbofan for high... 
Hybrid engines | Rocket engines
eJournal
SAE technical paper series, Volume 2004-01-3220.
This paper presents the steps involved in developing safety critical embedded control software for aerospace applications for the control of propulsion system.... 
Electronic control systems | Gas turbines | Rocket engines
eJournal
SAE technical paper series, Volume 730359.
.... With the engine and inlet operating at higher levels of performance, the need for improvements in control system technology has become more evident... 
Rocket engines | Turbojet 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... 
Rocket engines
eJournal
SAE technical paper series, Volume 2000-01-5602.
...: combined-cycle airbreathing/rocket engines. TSTO configurations were also established as conventional all-rocket and all-airbreathing engine comparison cases... 
Scramjet engines | Rocket engines
eJournal
SAE technical paper series, Volume 700798.
...). Performance of the engine and vehicle require engines with high expansion ratio nozzles in compact sizes... 
Launch vehicles | Rocket engines
eJournal
SAE technical paper series, Volume 881202.
Sustained high speed flight cannot be achieved by improvements in traditional turbojet/turbofan propulsion systems. Instead, propulsion cycles optimized for... 
Scramjet engines | Hybrid engines | Rocket engines | Turbojet engines
eJournal
SAE technical paper series, Volume 872348.
This paper addresses the effect of bypass ratio on thrust-to-weight, fuel flow, and hover efficiency. Four selected representative tilt propulsion system... 
Rocket engines | Turbojet engines
eJournal
SAE technical paper series, Volume 900995.
In the parametric optimization of an accelerator or a cruise vehicle for hypervelocity missions, five elements of the analysis relate to (i) vehicle... 
Hybrid engines | Rocket engines
eJournal
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