Deployable aeroshell flexible thermal protection system testing

20th AIAA Aerodynamic Decelerator Systems Technology Conference

Volumn , Issue , 2009, Pages

  Hughes, Stephen J ^a,d   Ware, Joanne S ^b   Corso, Joseph A Del ^a,d   Lugo, Rafael A ^c  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Materials Development Group   (United States)

^c NATIONAL INSTITUTE OF AEROSPACE   (United States)

^d NASA LaRC/MS 432   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; BALLISTICS; FIXTURES (TOOLING); HEAT FLUX; HEAT SHIELDING; LOCATION; MOUNTINGS; NASA; THERMAL INSULATING MATERIALS;

AERODYNAMIC LOADING; AEROTHERMAL HEATING; BALLISTIC COEFFICIENT; NASA LANGLEY RESEARCH CENTER; SIMULATION ANALYSIS; TECHNOLOGY READINESS LEVELS; TEST CONFIGURATIONS; THERMAL PROTECTION SYSTEM;

SURFACE TESTING;

EID: 77958164436     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-2926     Document Type: Conference Paper

References (4)

1. Harvin, S.F., Cabell, K.F., Mekkes, G.L., and Gallimore, S.D., "Test Capability Enhancements to the NASA Langley 8-Foot High Temperature Tunnel," JANNAF, 2006.
2. Ferlemann, P.G. "Analysis of the Material Test Sled During Injection into the 8'HTT Test Flow", Technical Note 05-523, TEAMS Contract NNL07AA00B, NASA Langley Research Center, October 29, 2008.
3. Del Corso, J.A., Bruce, W.E., Liles, K.A., and Hughes, S.J., "Thermal Analysis and Testing of Candidate Materials for PAIDAE Inflatable Aeroshell," AIAA, ADS Conference, May 2009.
4. Player, Charles, "PAIDAE Thermal Protection System Testing Final Report - FY2008," PAI-DAE-3.3-012, NASA Langley Research Center, 2008.