NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Some Shell Stability Problems in Missile and Space Vehicle AnalysisA brief discussion is presented of three structural shell stability studies in progress at Lockheed Missiles & Space Company: the stabilizing influence of solid propellants, the effect of cushion stiffness on buckling under cushion loading, and the snap-through buckling of axially loaded cylinders. Recent analytical results are compared with test data. Also included is a brief description of a few shell stability problems of present interest to LMSC for which satisfactory methods of analysis are not available.
Document ID
19630000934
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
D. O. Brush (Lockheed Missiles and Space Company Sunnyvale, California, United States)
Date Acquired
August 1, 2013
Publication Date
October 24, 1962
Publication Information
Publication: Collected Papers on Stability of Shell Structures - 1962
Publisher: National Aeronautics and Space Administration
Volume: Technical Note: D-1510
Issue Publication Date: December 1, 1962
Subject Category
Structural Mechanics
Mechanical Engineering
Meeting Information
Meeting: NASA Symposium on Instability of Shell Structures
Location: Hampton, VA
Country: US
Start Date: October 24, 1962
End Date: October 25, 1962
Sponsors: Langley Research Center
Accession Number
63N10808
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
MISSILE
SPACE VEHICLE
SHELL STABILITY

Related Records

IDRelationTitle19630000930WorkCollected Papers on Stability of Shell Structures - 1962
No Preview Available