Qualification Test for the Multiple Satellite Dispenser 0.2 lbf Rocket Engine Assembly REA 10-16,

Abstract

The report presents the results of a Qualification Test Program on Hamilton Standard Rocket Engine Assembly Model 10-16, a nominal 0.2 pound thrust monopropellant engine. The purpose of this test program was to demonstrate that this engine meets the performance and environmental requirements of the Naval Research Laboratories specification, NRL RFP N00014-73-R-0011, Part II.

Document Details

Document Type
Technical Report
Publication Date
Oct 15, 1973
Accession Number
AD0783188

Entities

People

  • A. E. Francis Sr

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Artificial Satellites
  • Assembly
  • Buildings And Structures
  • Dispensers
  • Engines
  • Military Research
  • Monopropellants
  • Qualifications
  • Research Facilities
  • Rocket Engines
  • Rockets
  • Specifications
  • Standards

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Aerospace Propulsion Engineering.
  • Software Engineering

Technology Areas

  • Space
  • Space - Hall-Effect Thruster