NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Performance equations for advanced orbital debris shieldsThis paper provides meteoroid and debris shield equations that have been developed at the NASA Johnson Space Center Hypervelocity Impact Test Facility. These equations define the performance capability of various types of meteoroid and debris shielding systems. Specific equations are applicable for aluminum Whipple shields, Nextel Multi-Shock (MS) shields, and Mesh Double-Bumper (MDB) shields. The MS and MDB shields are advanced shields with demonstrated weight and performance advantages over conventional Whipple shields.
Document ID
19920055960
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Christiansen, Eric L.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 15, 2013
Publication Date
March 1, 1992
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 92-1462
Report Number: AIAA PAPER 92-1462
Accession Number
92A38584
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available