Test Plan for Aerodynamic Heating and Pressure Tests of a 9-Percent Gemini B Re-Entry Configuration Model in the McDonnell Hypervelocity Impulse Tunnel,

Abstract

The purpose of this report is to present a test plan for thermodynamic heat transfer and pressure tests of a 9-percent Gemini B model in the hypervelocity impulse tunnel. The model will have interchangeable re-entry module-adapter interconnect fairings which will simulate the NASA Gemini and Gemini B configurations. (Author)

Document Details

Document Type
Technical Report
Publication Date
Feb 24, 1967
Accession Number
AD0856749

Entities

People

  • M. A. Haefner

Organizations

  • McDonnell Aircraft Corporation

Tags

DTIC Thesaurus Topics

  • Aerodynamic Heating
  • Energy
  • Energy Transfer
  • Heat Energy
  • Heat Transfer
  • Heating
  • Thermodynamics

Readers

  • Aerodynamics/Aeronautics.
  • Combustion and Flow Dynamics.
  • Manufacturing Engineering.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow