Bonding requirements in general are discussed. The additional factors that are introduced for spacecraft bonding are examined and shown to require methods that are outside of normal bonding techniques. An electronic box in a spacecraft is used to illustrate the problems encountered.
Unique bonding methods for spacecraft
Verbindungsverfahren fuer Raumfahrzeuge
1988
6 Seiten
Conference paper
English
SWAS Spacecraft T/V Test, Unique Chamber Tests Systems Actuation
British Library Conference Proceedings | 1997
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