Oxidizer heat exchanger component testing [PDF]
As part of the RL10 Rocket Engine Product Improvement Program, Oxidizer Heat Exchanger (OHE) stages 1, 2, and 3 were designed and fabricated during late 1983 and early 1984.
Kanic, P., Kmiec, T.
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Orbit transfer rocket engine technology program. Phase 2: Advanced engine study [PDF]
In Phase 2 of the Advanced Engine Study, the Failure Modes and Effects Analysis (FMEA) maintenance-driven engine design, preliminary maintenance plan, and concept for space operable disconnects generated in Phase 1 were further developed.
Erickson, C., Hines, B., Martinez, A.
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An experiment to detect microorganisms in the upper atmosphere flown on Aerobee NASA 4.150 [PDF]
Upper atmospheric microorganism detection by modified dust collector on Aerobee ...
Picciolo, G. L. +2 more
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Rocket base flow field studies using an electron beam probe Quarterly progress report no. 1, 25 Jun. - 25 Sep. 1965 [PDF]
Electron beam probe used in rotational temperature measuring apparatus - rocket base flow ...
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Small Engine Component Technology (SECT) [PDF]
A study of small gas turbine engines was conducted to identify high payoff technologies for year-2000 engines and to define companion technology plans.
Benn, K. +4 more
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IXPE Mirror Module Assemblies [PDF]
Expected to launch in 2021 Spring, the Imaging X-ray Polarimetry Explorer (IXPE) is a NASA Astrophysics Small Explorer Mission with significant contributions from the Italian space agency (ASI).
Alexander, Cheryl +14 more
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Rocket-miR, a translational launchpad for miRNA-based antimicrobial drug development. [PDF]
Neff SL +6 more
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Study of solid rocket motor for a space shuttle booster. Appendix B: Typical component recertification test procedures [PDF]
Flexseal assemblies, TVC actuators, hydraulic supply system, TVC electronic control unit, flight instrumentation system, ordnance system electronics, and hydrotest of SRM case segments are discussed, applied to typical component recertification test ...
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High temperature NASP engine seal development [PDF]
Key to the development of advanced hypersonic engines such as those being considered for the National Aerospace Plane (NASP) is the development and evaluation of high temperature, flexible seals that must seal the many feet of gaps between the ...
Melis, Matthew E. +3 more
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Particle size of aluminum oxide produced by a small rocket motor [PDF]
Spectrophotometric method for measurement of aluminum oxide particle sizes during burning of solid propellant rocket ...
Dobbins, R. A.
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