Accession Number:

AD0843200

Title:

WS 107A-1 Flight Test Working Group, Flight Test Report, Atlas Missile 32E

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

Report Date:

1961-11-17

Pagination or Media Count:

71.0

Abstract:

The primary purposes of the flight were to obtain data for determining the performance of the Propellant Utilization System and to evaluate the Inertial Guidance System Performance.

Descriptors:

• *SURFACE TO SURFACE MISSILES
• FLIGHT CONTROL SYSTEMS
• FAILURE
• LIQUID PROPELLANT ROCKET ENGINES
• HYDRAULIC EQUIPMENT
• DESTRUCTORS
• LIQUID ROCKET OXIDIZERS
• PNEUMATIC EQUIPMENT
• SUSTAINER ENGINES
• PRESSURE REGULATORS
• PROPELLANT CONTROL
• ABORT
• FLIGHT TESTING
• INERTIAL GUIDANCE

Subject Categories:

• Surface-Launched Guided Missiles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE