Results 151 to 160 of about 190,559 (293)
Development of Combustion Test Facility for Liquid Rocket Engine [PDF]
, 2006 Dong-Hwan Kim +2 more
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Determination of the effects of nozzle nonlinearities upon nonlinear stability of liquid propellant rocket motors [PDF]
The research is reported concerning the development of a three-dimensional nonlinear nozzle admittance relation to be used as a boundary condition in the nonlinear combustion instability theories for liquid propellant rocket engines.
Padmanabhan, M. S. +2 more
core +1 more source
Rotordynamic Analysis of a High Thrust Liquid Rocket Engine Turbopump [PDF]
, 2008 Seong-Min Jeon +3 more
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Test stand design and analysis for Titan 34D static firing [PDF]
The Test Stand 1C at the Air Force Astronautic Laboratory (AFAL), Edwards AFB, Calif., was originally designed for F-1 liquid propellant engines. The stand was modified to handle a five and one half segment Solid Rocket Motor (SRM) Titan 34D vertical ...
Pazargadi, Shayan
core +1 more source
Dual-fuel, dual-mode rocket engine [PDF]
, 1989 The invention relates to a dual fuel, dual mode rocket engine designed to improve the performance of earth-to-orbit vehicles. For any vehicle that operates from the earth's surface to earth orbit, it is advantageous to use two different fuels during its ...
Martin, James A.
core +1 more source
, 2008 Control over drop size distributions, injection rates, and geometrical distribution of fuel and oxidizer sprays in bi-propellant rocket engines has the potential to produce more efficient, more stable, less polluting rocket engines.
Bramanti, Cristina +4 more
core +1 more source
Erratum to: “Numerical and experimental investigations of the effect of repeated cyclic thermal loads on the strength of materials of recoverable liquid-propellant rocket engines” [PDF]
, 2009 V. I. Bubnov +3 more
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Spray combustion under oscillatory pressure conditions [PDF]
The performance and stability of liquid rocket engines is often argued to be significantly impacted by atomization and droplet vaporization processes.
Jacobs, H. R., Santoro, R. J.
core +1 more source
, 1981 The system includes reusable turbojet propelled booster vehicles releasably connected to a reusable rocket powered orbit vehicle. The coupled orbiter-booster combination takes off horizontally and ascends to staging altitude and speed under booster power
Jackson, L. R. +3 more
core +1 more source
Distributed Health Monitoring System for Reusable Liquid Rocket Engines [PDF]
, 2010 Ching-Fang Lin +3 more
openalex +1 more source