Accession Number:

AD0835521

Title:

FLIGHT READINESS FIRING TEST. CONVAIR TEST NUMBER P3-402-00-17 AMR RANGE TEST NUMBER 2676 9 SEPTEMBER 1959 SERIES D ARTICLE 17,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

• O'Dell, H. C.

Report Date:

1959-09-18

Pagination or Media Count:

102.0

Abstract:

This report has been prepared to present test data and test results from the Flight Readiness Firing of XSM-65D Missile No. 17 at Complex 13, AMR. Author

Descriptors:

• *SURFACE TO SURFACE MISSILES
• LIQUID PROPELLANT ROCKET ENGINES
• FLIGHT TESTING
• ENGINE CLUSTERS
• CAPTIVE TESTS
• SUSTAINER ENGINES
• BOOSTER ROCKET ENGINES
• VERNIER ROCKET ENGINES
• PITCH(MOTION)
• ROLL
• YAW
• GUIDED MISSILE TRACKING SYSTEMS
• GIMBALS
• LIQUID ROCKET OXIDIZERS
• PROPELLANT TANKS
• PRESSURIZATION
• PROPELLANT CONTROL
• HYDRAULIC EQUIPMENT
• FLIGHT CONTROL SYSTEMS
• PNEUMATIC EQUIPMENT
• IMPACT PREDICTION
• GUIDED MISSILE RANGES
• PERFORMANCE(ENGINEERING)

Subject Categories:

• Surface-Launched Guided Missiles
• Liquid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE