X-34 Experimental Aeroheating at Mach 6 and 10
نویسندگان
چکیده
منابع مشابه
Aeroheating Characteristics for a Two-Stage-To-Orbit Concept During Separation at Mach 6
An experimental study was conducted to determine the proximity aeroheating characteristics for a two-stage-to-orbit concept in close proximity in the NASA Langley 20-Inch Mach 6 Air Tunnel. A new hybrid discrete thin-film resistance gauge technique was evaluated in this study and used to measure experimental interference heating levels between the booster and the orbiter at a constant freestrea...
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The goal of the NASA Reusable Launch Vehicle (RLV) technology program is to develop and demonstrate essential, cost-effective technologies for next-generation launch systems. The XÐ33 flight vehicle presently being developed by Lockheed-Martin is an experimental Single-Stage-to-Orbit (SSTO) demonstrator that is intended to validate critical technologies for the full-scale RLV. One of the key te...
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ژورنال
عنوان ژورنال: Journal of Spacecraft and Rockets
سال: 1999
ISSN: 0022-4650,1533-6794
DOI: 10.2514/2.3447