Preliminary Flight Rating Tests of the HAST Propulsion System

Abstract

Preliminary Flight Rating Tests of the hybrid rocket propulsion system for the HAST target missile were accomplished by the Air Force Rocket Propulsion Laboratory. Nine tests of the flight configuration system were conducted at simulated altitude. Overall operating characteristics and performance were shown to be satisfactory for missile flight tests.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1975
Accession Number
ADA012200

Entities

People

  • Carlton D. Penn
  • John E. Branigan

Organizations

  • Air Force Research Laboratory

Tags

Communities of Interest

  • Ground and Sea Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Contractors
  • Contracts
  • Data Acquisition
  • Engineers
  • High Altitude
  • Ignition
  • Material Degradation Processes
  • Materials Laboratories
  • Materials Processing
  • Measurement
  • Plastic Explosives
  • Pressure Measurement
  • Pressure Regulators
  • Pressurization
  • Propulsion Systems
  • Rocket Propulsion
  • Test Facilities

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Missile Defense Systems.