Z(WS 107A-1)ZFlight Test Working Group Flight Test Report Atlas Missile 25E 2 October 1961 AMR Range Test Number 1252, Astronautics Test Number P1-503-00-25.

Abstract

First order objectives of the flight included obtaining data on the re-entry vehicle impact location for the statistical determination of CEP, the evaluation of the flight control system performance, the evaluation of the inertial guidance system performance and accuracy and the evaluation of the performance of the acoustica PU system. (Author)

Document Details

Document Type
Technical Report
Publication Date
Oct 06, 1961
Accession Number
AD0843303

Entities

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Astronautics
  • Control Systems
  • Flight Control Systems
  • Guidance
  • Inertial Navigation
  • Inertial Navigation Systems
  • Navigation
  • Test And Evaluation

Fields of Study

  • Physics

Readers

  • Aerospace Test and Evaluation

Technology Areas

  • Space