Accession Number:

AD0775607

Title:

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

Descriptive Note:

Engineering rept.,

Corporate Author:

HAMILTON STANDARD WINDSOR LOCKS CONN

Personal Author(s):

Report Date:

1973-11-07

Pagination or Media Count:

197.0

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.

Subject Categories:

  • Liquid Propellant Rocket Engines
  • Unmanned Spacecraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE