Accession Number:

AD0772489

Title:

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

Descriptive Note:

Corporate Author:

HAMILTON STANDARD WINDSOR LOCKS CONN

Personal Author(s):

Report Date:

1973-12-10

Pagination or Media Count:

196.0

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.

Subject Categories:

  • Liquid Propellant Rocket Engines
  • Unmanned Spacecraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE