Published 1986 | Version v1
Book

System structural test results: six PODS III supports

  • 1. Lockheed Missiles and Space Co., Palo Alto, CA

Description

Passive orbital disconnect struts can potentially reduce the support conductance a factor of 10 over state-of-the-art tension band nondisconnect supports and cut helium dewar weights in half for the same lifetime. A series of thermal and structural tests were performed to verify that this performance improvement is real. Structural tests on a PODS-III support system (consisting of six struts) is reported here. The results show the predicted performance improvements can be achieved and the PODS-III supports are ready for flight applications. For large tankage systems requiring higher side load capability, a PODS-IV version is currently being developed

Additional details

Publishing Information

Publisher
Plenum Press.
Imprint Place
New York, NY (USA)
Imprint Title
Advances in cryogenic engineering: Vol. 31
Journal Page Range
p. 941-948.

Conference

Title
Cryogenic engineering conference and international cryogenic materials conference.
Dates
12-16 Aug 1985.
Place
Boston, MA (USA).

INIS

Country of Publication
United States
Country of Input or Organization
United States
INIS RN
18016901
Subject category
S71: CLASSICAL AND QUANTUM MECHANICS, GENERAL PHYSICS;
Resource subtype / Literary indicator
Conference
Descriptors DEI
COOLING SYSTEMS; CRYOGENICS; DEWARS; FATIGUE; HYDRAULICS; LIFETIME; MECHANICAL TESTS; PERFORMANCE; SPACE VEHICLES; STRUCTURAL MODELS; SUPPORTS; TANKS; THERMAL EXPANSION; THERMAL TESTING
Descriptors DEC
CONTAINERS; EXPANSION; MATERIALS TESTING; MECHANICAL PROPERTIES; MECHANICAL STRUCTURES; NONDESTRUCTIVE TESTING; TESTING