Optimal Design of Fuel-Rich Gas Generator for Liquid Rocket Engine [PDF]
, 2004 Sun-Tak Kwon, Changjin Lee
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Fiber-reinforced ceramic composites for Earth-to-orbit rocket engine turbines [PDF]
Fiber reinforced ceramic matrix composites (FRCMC) are emerging materials systems that offer potential for use in liquid rocket engines. Advantages of these materials in rocket engine turbomachinery include performance gain due to higher turbine inlet ...
Brockmeyer, Jerry W. +1 more
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Theory and Design of Flight-Vehicle Engines [PDF]
Papers are presented on such topics as the testing of aircraft engines, errors in the experimental determination of the parameters of scramjet engines, the effect of the nonuniformity of supersonic flow with shocks on friction and heat transfer in the ...
Kurziner, R. I., Zhdanov, V. T.
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Pitch Plane Trajectory Tracking Control for Sounding Rockets via Adaptive Feedback Linearization [PDF]
arXivThis paper proposes a pitch plane trajectory tacking control solution for suborbital launch vehicles relying on adaptive feedback linearization. Initially, the 2D dynamics and kinematics for a single-engine, thrust-vector-controlled sounding rocket are obtained for control design purposes.
arxiv
Combustion Characteristics of Fuel-rich Gas Generator with Impinging Injector for a Liquid Rocket Engine [PDF]
, 2005 Yeoung-Min Han +5 more
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Tank construction for space vehicles Patent [PDF]
, 1967 Liquid propellant tank design with semitoroidal ...
Blumrich, J. F., Loy, C. A.
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Radial Turbine Preliminary Aerodynamic Design Optimization for Expander Cycle Liquid Rocket Engine [PDF]
, 2006 Yolanda Mack +6 more
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Cryostatless high temperature supercurrent bearings for rocket engine turbopumps [PDF]
The rocket engine systems examined include SSME, ALS, and CTV systems. The liquid hydrogen turbopumps in the SSME and ALS vehicle systems are identified as potentially attractive candidates for development of Supercurrent Bearings since the temperatures ...
Dill, James F., Rao, Dantam K.
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, 1977 An accumulator particularly adapted for use in controlling the pressure of a stream of fluid in its liquid phase utilizing the fluid in its gaseous phase was designed.
Fenwick, J. R., Karigan, G. H.
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Performance prediction method of multi-stage steam ejector system in high-altitude simulation test
AIP AdvancesThe Multi-Stage Steam Ejector System (MSSES) is essential for High-Altitude Simulation Tests (HASTs) of liquid rocket engines using active ejection. Rapid performance prediction is crucial due to the system’s high energy consumption.
Lide Chao +4 more
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