Aerospace Expandable Stuctures. Conference Transactions
Report Number: AFAPL TR 65-108
Corporate Author(s): Air Force Aero Propulsion Laboratory
Date of Publication: 1965-05-27
Pages: 803
DoD Task:
Identifier: AD0631406
Abstract:
The report is based upon the discussions at the Conference held at the Lafayette Club, Minnetonka Beach, Minnesota. The subject matter has been arranged in six sessions in the order of presentation at the conference, followed by six papers which were not given at the conference.
Provenance: Lockheed Martin Missiles & Fire Control
Corporate Author(s): Air Force Aero Propulsion Laboratory
Date of Publication: 1965-05-27
Pages: 803
DoD Task:
Identifier: AD0631406
Abstract:
The report is based upon the discussions at the Conference held at the Lafayette Club, Minnetonka Beach, Minnesota. The subject matter has been arranged in six sessions in the order of presentation at the conference, followed by six papers which were not given at the conference.
Provenance: Lockheed Martin Missiles & Fire Control
Other options for obtaining this report:
Via the Defense Technical Information Center (DTIC): A record for this report, and possibly a pdf download of the report, exists at DTIC Via National Technical Report Library: This report may be available for download from NTRL. Use the Title from this record to locate the item in DTIC Online Indications of Public Availability No digital image of an index entry indicating public availability is currently available There has been no verification of an indication of public availability from an inside cover statementRelated report(s):
This conference contains the following reports:
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Introduction and Table of Contents
AFAPL TR 65-108 p. i-xiii -
Expandable Structures Design Concepts for Astronaut Transfer
AFAPL TR 65-108 p. 1-18 -
Development and Opitimization of Resin Systems
for Expandable Honeycomb
AFAPL TR 65-108 p. 19-50 -
Application of Expandable Honeycomb to Fabrication of Space Structures
AFAPL TR 65-108 p. 50-73 -
Lightweight, Expandable Support Shelter Systems
AFAPL TR 65-108 p. 75-103
-
Bare Base Development Concepts
AFAPL TR 65-108 p. 104-139 -
'Ratio' Automated Assembly Technique for Space Structures
AFAPL TR 65-108 p. 141-163 -
Chemical Rigidization of Preformed Flexible Foams
AFAPL TR 65-108 p. 165-178 -
Maintenance Technology for Space Systems
AFAPL TR 65-108 p. 179-197 -
Structural Considerations for an Expandable Lenticular Satellite
AFAPL TR 65-108 p. 199-213 -
Application of Inflatable Structures to Station Keeping of Passive Communications Satellites
AFAPL TR 65-108 p. 215-233 -
Development of Manufacturing Techniques for a Metal Fabric Reinforced Re-entry Paraglider
AFAPL TR 65-108 p. 235-247 -
Bending of Unfurlable Tubular Structures in Space
AFAPL TR 65-108 p. 249-263 -
Development and Evaluation of a Rigidized Inflatable Microwave Reflector
AFAPL TR 65-108 p. 265-287 -
Sodium Silicate as a Versatile Structural Material
AFAPL TR 65-108 p. 289-303 -
Inflatable Thermal Radiation Shield for Space Application
AFAPL TR 65-108 p. 305-338 -
Predistributed Foam for Rigidizing Membrane Structures in Space
AFAPL TR 65-108 p. 339-361 -
Semi-rigid Structures for Space Applications: Expandable Space Structure
AFAPL TR 65-108 p. 362-395 -
Buildings in Barrels, Part III
AFAPL TR 65-108 p. 397-428 -
Metal Fabrics for Aerospace Expandable Structures
AFAPL TR 65-108 p. 429-446 -
Simulation of Meteoroid Impact Effects on Expandable Structures
AFAPL TR 65-108 p. 447-466 -
Development of an Expandable Airlock Utilizing the Elastic Recovery Principle
AFAPL TR 65-108 p. 467-496 -
Potential Applications for Expandable and Inflatable Structures for Re-entry Vehicles
AFAPL TR 65-108 p. 497-518 -
Compression Tests of Wire-Film Cylinders
AFAPL TR 65-108 p. 519-535 -
Design Criteria for Inflated, Expandable Beams Used as Structural Members in an Advanced Concept Paraglider
AFAPL TR 65-108 p. 537-554 -
Development of Space Expanded and Rigidized Solar Energy Collectors
AFAPL TR 65-108 p. 555-571 -
Aluminum Foil Expandable Structures
AFAPL TR 65-108 p. 572-602 -
Fabrication and Pressurization Technology for Improvement of Surface Accuracy of Passive Communications Satellites
AFAPL TR 65-108 p. 603-616 -
Membrane Analysis of Pressurized Thin Spheroid Shells Composed of Flat Gores and Its Application to Echo II
AFAPL TR 65-108 p. 617-631 -
Astronaut Maneuvering Unit Technology
AFAPL TR 65-108 p. 633-648 -
Deployment System for the Pegasus Meteoroid Technology Satellite
AFAPL TR 65-108 p. 649-657 -
Structural Behavior of Tapered Inflated Fabric Cylinders Under Various Loading Conditions
AFAPL TR 65-108 p. 659-685 -
Satellite Applications for Expandable Space Structures
AFAPL TR 65-108 p. 687-707 -
Recent Applications of Inflated Structures to Aerospace Vehicles
AFAPL TR 65-108 p. 709-739 -
Correlation of Analytical and Experimental Results of Cylindrical Shells Under Newtonian Pressure Distribution
AFAPL TR 65-108 p. 740-767 -
High-Temperature Protective Re-entry Coatings for Expandable Structures
AFAPL TR 65-108 p. 769-783 -
Dual Wall Inflatable Structures for Space Oriented Applications
AFAPL TR 65-108 p. 785-802