Accession Number:

AD0832664

Title:

STRESS ANALYSIS-2ND STAGE AIRFRAME-FORWARD SECTION. USAF MODEL XSM-65D,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

• Beatty, J. W.

Report Date:

1958-11-20

Pagination or Media Count:

283.0

Abstract:

The following stress analysis report proves the Second Stage Airframe of the XSM-65D, R and D and I.O.C. Missiles forward of station 522 to be structurally adequate for all load conditions occurring during the ground handling and flight of the missile. Author

Descriptors:

• *SURFACE TO SURFACE MISSILES
• AIRFRAMES
• STRESSES
• STRUCTURAL PROPERTIES
• RELIABILITY
• LOADS(FORCES)
• TENSILE PROPERTIES
• SHEAR STRESSES
• COMPRESSIVE PROPERTIES
• BENDING
• NOSE CONES
• SEPARATION
• ADAPTERS
• WALLS
• PROPELLANT TANKS
• PROPELLANT CONTROL
• PIPES
• JOINTS
• BOOSTER ROCKET ENGINES

Subject Categories:

• Surface-Launched Guided Missiles
• Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE