Technologies for thermal protection systems applied on reusable launcher

54th International Astronautical Congress of the International Astronautical Federation (IAF), the International Academy of Astronautics and the International Institute of Space Law

Volumn 2, Issue , 2003, Pages 619-626

  Behrens, Burkhard ^a   Müller, Mark ^a  

^a AIRBUS GROUP INNOVATIONS   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

CARBON; COMPUTATIONAL FLUID DYNAMICS; COSTS; LAUNCHING; OPTIMIZATION; ORBITS; RESEARCH; REUSABILITY; SILICON CARBIDE; THERMAL INSULATION;

PAYLOADS; REUSABLE LAUNCH VEHICLE (RLV); SUB-ORBITAL HOPPERS; THERMAL PROTECTION SYSTEM (TPS);

SPACE FLIGHT;

EID: 22344438583     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (3)

1. Behrens, B.: Thermal Protection and Hot Structures for Re-usable Launch Systems, 3rd European Conference on Launcher Technology, Strasbourg, December 2001
2. Fischer, W.P.P.; Behrens, B.: Development Status of TPS Candidates for Future RLV's, 3rd International Symposium Atmospheric Reentry Vehicles and Systems, Arcachon, March 2003
3. FSS-RIBRE-PRE-0002-02, ASTRA Zwischenbericht zu AP140, 21.11.2002