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, Model 16-10, a nominal 0.2 pound thrust monopropellant engine. The purpose of the tests performed was to establish engine characteristics over extended life and to establish performance parameters over a range of operating conditions.

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Document Details

Document Type
Technical Report
Publication Date
Nov 07, 1973
Accession Number
AD0775607

Entities

People

  • William W. Arkilander

Organizations

  • United Technologies Corporation

Tags

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Aerospace Propulsion Engineering.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster