Overstress Qualification Test of the Multiple Satellite Dispenser 5 LBF Rocket Engine Assembly REA 16-9,

Abstract

The report presents the results of a portion of a Qualification Overstress Test on Hamilton Standard Rocket Engine Assembly, Model 16-9, a nominal 5.0 pound thrust monopropellant engine. The objectives of this portion of the Qualification Overstress Tests were to characterize the engine over extended life and at various operating conditions.

Document Details

Document Type
Technical Report
Publication Date
Dec 10, 1973
Accession Number
AD0772489

Entities

People

  • Joseph Genovese

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Artificial Satellites
  • Assembly
  • Dispensers
  • Engines
  • Monopropellants
  • Qualifications
  • Rocket Engines
  • Rockets
  • Standards

Fields of Study

  • Physics

Readers

  • Aerospace Propulsion Engineering.
  • Software Engineering

Technology Areas

  • Space
  • Space - Hall-Effect Thruster