THOR MB-3 QUARTERLY FLIGHT.

Abstract

A composite analysis of first-stage propulsion system operation during all Thor space booster flights is presented for the period from 1 April 1963 through 19 June 1963. The Atlantic Missile Range and the Pacific Missile Range were used for the launch activity. Configuration of each Thor vehicle launch during the report period is presented and a summary of telemetered perform ance data is included. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jul 30, 1963
Accession Number
AD0411168

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Composite Materials
  • Engineering
  • Propulsion Systems

Readers

  • Aerospace Test and Evaluation
  • Nanocomposite Materials Science
  • Technical Research and Report Writing.

Technology Areas

  • Space