A payload retention concept that may be utilized on Space Shuttle missions is investigated. This concept appears to embody all the desirable features for the very demanding requirements for space flight. Desirable features include light weight, low cost, high reliability, excellent load distribution, versatility, and insensitivity to critical alignment.
STS payload retention system concept
1982-09-01
Report
No indication
English
STS Payload Retention System Concept
NTIS | 1982
|NTRS | 1992
|Hemispherical Latching Apparatus for Payload Retention
NTIS | 1982
|