Accession Number:

AD0842791

Title:

Evaluation Test of Fuel Duct Assembly Booster Engine No. 2 Convair Drawing Nos. 27-21141-1 and 27-21105-801.

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

• Richesin, I. J.

Report Date:

1960-08-16

Pagination or Media Count:

40.0

Abstract:

The object of this test was to determine the structural integrity of a booster engine fuel duct assembly during design proof, static load, flex, vibration and burst tests. Author

Descriptors:

• *BOOSTER ROCKET ENGINES
• *DUCT INLETS
• PROPELLANT TRANSFER
• STRUCTURAL PROPERTIES
• LIQUID PROPELLANT ROCKET ENGINES
• DUCTS
• SUPPORTS
• VALVES
• DISCONNECT FITTINGS
• LOADS(FORCES)
• FLEXIBLE STRUCTURES
• TURBOPUMPS
• FLANGES
• VIBRATION
• RUPTURE
• STAGING
• TEST EQUIPMENT
• PRESSURIZATION

Subject Categories:

• Pumps, Filters, Pipes, Tubing, Fittings and Valves
• Mechanics
• Liquid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE