Accession Number:

AD0772491

Title:

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

Descriptive Note:

Standard engineering rept.,

Corporate Author:

HAMILTON STANDARD WINDSOR LOCKS CONN

Personal Author(s):

Report Date:

1973-11-01

Pagination or Media Count:

41.0

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.

Subject Categories:

  • Liquid Propellant Rocket Engines
  • Unmanned Spacecraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE