Accession Number:

AD0832458

Title:

DYNAMIC RESPONSE CHARACTERISTICS OF 'D' SERIES FLIGHT CONTROL SYSTEM BOOSTER SECTION VERSION 27-7001 IN TSTS NO. 2, WS 107A,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

• Tate, J. C.

Report Date:

1959-08-14

Pagination or Media Count:

62.0

Abstract:

The object of this test was to obtain dynamic preflight information for the Series D Flight Control System. Author

Descriptors:

• *FLIGHT CONTROL SYSTEMS
• *SURFACE TO SURFACE MISSILES
• ATTITUDE CONTROL SYSTEMS
• DYNAMICS
• STABILITY
• RESPONSE
• HYDRAULIC EQUIPMENT
• BOOSTER ROCKET ENGINES
• HYDRAULIC SERVOMECHANISMS
• STABILIZATION SYSTEMS
• DETECTORS
• FEEDBACK
• CAPTIVE TESTS

Subject Categories:

• Surface-Launched Guided Missiles
• Liquid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE