Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m2 (350 psia) [PDF]
The joint Army. Navy, NASA. Air Force (JANNAF) rocket engine peformnace prediction procedure is based on the use of various reference computer programs. One of the reference programs for nozzle analysis is the Two-Dimensional Kinetics (TDK) Program.
Kacynski, Kenneth J. +2 more
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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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Electro-thermal rocket Patent [PDF]
, 1962 Electrothermal rocket engine using resistance heated heat ...
Jack, J. R., Moeckel, W. E.
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Single-Cycle Impulse from Detonation Tubes with Nozzles [PDF]
, 2008 Experiments measuring the single-cycle impulse from detonation tubes with nozzles were conducted by hanging the tubes in a ballistic pendulum arrangement within a large tank.
Cooper, M., Shepherd, J. E.
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The needs of the designer of a solid core nuclear rocket engine are discussed. Some of the topics covered include: (1) a flight thrust module/feed system module assembly; (2) a nuclear thermal rocket (NTR), expander cycle, dual T/P; (3) turbopump ...
Gunn, Stanley
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An Experimental Study of the Performance of a Subscale Kerosene - Fuelled Ejector Ramjet at Simulated Takeoff [PDF]
, 1996 The ejector ramjet is a rocket based combined cycle propulsion system in which a rocket and ramjet are integrated to accrue synergistic benefits. A proof-of-concept experiment to augment the thrust of a simulated rocket by the induction of air through ...
Isaac, JJ +7 more
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The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios [PDF]
, 1994 Kenneth J. Kacynski, Joe D. Hoffman
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A detailed description of the uncertainty analysis for High Area Ratio Rocket Nozzle tests at the NASA Lewis Research Center [PDF]
A preliminary uncertainty analysis has been performed for the High Area Ratio Rocket Nozzle test program which took place at the altitude test capsule of the Rocket Engine Test Facility at the NASA Lewis Research Center.
Chuang, Isaac +2 more
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Gimbaled, partially submerged rocket nozzle Patent [PDF]
, 1965 Gimbaled partially submerged nozzle for solid propellant rocket engines for providing directional ...
Brown, R. L.
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DESIGN AND ANALYSIS OF AEROSPIKE BELL NOZZLE TO IMPROVE THRUST IN ROCKET ENGINE
, 2022 A J Sriganapathy +2 more
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