Technologies for thermal protection systems applied on re-usable launcher

Acta Astronautica

Volumn 55, Issue 3-9, 2004, Pages 529-536

  Behrens, Burkhard ^a   Müller, Mark ^a  

^a AIRBUS GROUP INNOVATIONS   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

CATAPULTS (AIRCRAFT LAUNCHERS); COMPUTATIONAL FLUID DYNAMICS; COSTS; HARDWARE; LAUNCHING; OPTIMIZATION; REUSABILITY; SPACECRAFT;

FLEXIBLE EXTERNAL INSULATIONS (FEI); REUSABLE LAUNCH VEHICLE (RLV); THERMAL PROTECTION SYSTEMS (TPS);

AEROSPACE ENGINEERING;

EID: 3843115485     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.actaastro.2004.05.034     Document Type: Conference Paper

References (3)

1. B. Behrens, Thermal protection and hot structures for re-usable launch systems, Third European Conference on Launcher Technology, Strasbourg, December 2001.
2. W.P.P. Fischer, B. Behrens, Development status of TPS candidates for future RLVs, Third International Symposium Atmospheric Reentry Vehicles and Systems, Arcachon, March 2003.
3. FSS-RIBRE-PRE-0002-02, ASTRA Zwischenbericht zu AP140, 21.11.2002.