Results 121 to 130 of about 11,111 (215)
Conjugate Analysis of Rocket Nozzle Ablation [PDF]
47th AIAA Thermophysics Conference, 2017 Peter G. Cross, Iain D. Boyd
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Preparation, Mechanical Properties and Strengthening Mechanism of W-Re Alloys: A Review. [PDF]
Materials (Basel), 2023 Zheng Z +5 more
europepmc +1 more source
Application of Ablation to a High Chamber Pressure Rocket Engine [PDF]
Ablation cooling in rocket engine with combustion chamber liner and nozzle constructed of silica phenolic ablative ...
Brecheisen, A. W., Ehresman, C. M.
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Solid Propulsion Integrity Program (SPIP) for verifiable enhanced solid rocket motor reliability [PDF]
To increase the success rate of U.S. built Rocket Motors (SRM), the approach taken is: (1) set common reliability goals for nozzles, cases, bondline, propellant, and insulation; (2) build a common engineering data base to support standard industry-wide ...
Butler, Barry L.
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Reliability of solid rocket motor cases and nozzles [PDF]
A recent article in Aerospace America claims that 'the average success ratio of the current U.S. stable of launch vehicles, including upper stages, is about 92 percent (without upper stages it is close to 95 percent).
Crose, James G.
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Atomization Characteristics of Hydrogen Peroxide Solutions in Electrostatic Field. [PDF]
Micromachines (Basel), 2022 Huang X, Sheng L, Lu Y, Li S.
europepmc +1 more source
High pressure water jet cutting and stripping [PDF]
High pressure water cutting techniques have a wide range of applications to the American space effort. Hydroblasting techniques are commonly used during the refurbishment of the reusable solid rocket motors.
Babai, Majid K., Hoppe, David T.
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Some investigations of heterogeneous flow in a rocket nozzle
, 1962 In the heterogeneous flow of finely divided particles and gas in a rocket nozzle, the assumptions that the flow enters the nozzle with no lags, that the radiative transport of energy between particles is negligible, and that there are no temperature gradients within the particles, are commonly made.
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NASP X-30 Propulsion technology status [PDF]
The performance goals of the NASP program require an aero-propulsion system with a high effective specific impulse. In order to achieve these goals, the high potential performance of air-breathing engines must be achieved over a very wide Mach number ...
Powell, William E.
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