Accession Number:

AD0262455

Title:

PARTIAL QUALIFICATION TEST OF TITAN I ENGINE COMPONENT THRUST CHAMBER ASSEMBLY CONTROLS, AEROJET-GENERAL CORPORATION, SACRAMENTO, CALIFORNIA

Descriptive Note:

Corporate Author:

WYLE LABS INC EL SEGUNDO CALIF

Personal Author(s):

• MORTENSON,L.N.
• CLARK,R.B.

Report Date:

1961-06-15

Pagination or Media Count:

1.0

Abstract:

Purpose of this program was to subject one assembly of the Titan I first stage thrust chamber controls to the flight simulation test phase of a qualification test program. A detailed description of the test program, along with the test equipment employed in the performance of the test program is included. Author

Descriptors:

• *COMBUSTION CHAMBERS
• *ROCKET ENGINES
• CALIBRATION
• CONTROL
• EXCITATION
• FLIGHT
• HIGH PRESSURE VALVES
• INSTRUMENTATION
• SIMULATION
• SURFACE TO SURFACE
• TEST EQUIPMENT
• TEST METHODS
• VALVES

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE