Overstress Qualification Test of the Multiple Satellite Dispenser 0.2 lbf Rocket Engine Assembly REA 10-16.

Abstract

The report presents the results of a portion of a qualification overstress test on Hamilton Standard Rocket Engine Assembly 10-16, a nominal 0.2 footpounds thrust hydrazine monopropellant engine. This phase of the testing was concerned with verification of nozzle thrust coefficients and critical soakback testing of the REA.

Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1973
Accession Number
AD0772491

Entities

People

  • William Arkilander

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Artificial Satellites
  • Assembly
  • Coefficients
  • Dispensers
  • Engines
  • Hydrazines
  • Monopropellants
  • Qualifications
  • Rocket Engines
  • Rockets
  • Standards
  • Verification

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Aerospace Propulsion Engineering.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster