Aeroheating Characteristics for a Two-Stage-To-Orbit Concept During Separation at Mach 6

  • Derek S. Liechty
  • Published 2005

Abstract

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… (More)

Topics

19 Figures and Tables

Cite this paper

@inproceedings{Liechty2005AeroheatingCF, title={Aeroheating Characteristics for a Two-Stage-To-Orbit Concept During Separation at Mach 6}, author={Derek S. Liechty}, year={2005} }