The aerothermodynamic measurement system of the X- 38

9th International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 1999, Pages

  Janovsky, R ^a   Romberg, O ^a   Tausche, M ^a   Wienss, W ^a  

^a OHB SYSTEM AG   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; FLIGHT SIMULATORS; HEAT FLUX; NASA; NUMERICAL METHODS; REENTRY; THERMAL INSULATION;

AEROTHERMODYNAMIC MEASUREMENT; DATA RECORDING SYSTEMS; EXTERNAL INSULATIONS; FLIGHT ENVIRONMENT; FLOW SIMILARITIES; MEASUREMENT SYSTEM; SURFACE TEMPERATURES; THERMAL PROTECTION SYSTEM;

HYPERSONIC VEHICLES;

EID: 85088768470     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-4817     Document Type: Conference Paper

References (5)

1. [RDl] X-38 Crew Return Vehicle Structural Design Loads Data Book, JSC-27725, Rev. 3, April 22nd 1998.
2. [RD2] Structural and Mechanical Verification Plan for the Experimental Crew Return Vehicle (X-CRV), JSC-27400.
3. [RD3] Spacecraft Structures and Mechanisms, Thomas P. Sarafin, pp. 405 ff., Kluwer Academic Publishers, 2nd rinting, 1997.
4. [RD4] Files BP's (ATDB) 10-98. xls&BP Heating (ATDB) 10-98. xls, X-38 Body-point location and local heat flux distribution at the surface of the X-38 during re-entry, Cycle-8 trajectory.
5. [RD5] TETRA, Technologies for Future Space Transportation Systems, Test Plan, Procedures and Report, TET-QHB-21-TP-7005, 21. 05. 99.