NOTES ON THE DESIGN AND PERFORMANCE OF A THREE-STAGE ROCKET TEST VEHICLE FOR AERODYNAMIC RESEARCH AT HYPERSONIC SPEEDS

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1961
Accession Number
AD0287540

Entities

People

  • J. A. Hamilton

Organizations

  • AGARD

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aircrafts
  • Altitude
  • Boost Phase
  • Boundary Layer
  • Elevation
  • Flight Paths
  • Fluid Dynamics
  • Free Flight
  • Frequency
  • Governments
  • Mach Number
  • Measurement
  • Nato
  • Rockets
  • Test Vehicles
  • Wind Tunnels

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow