The development of spacecraft loads, design and test philosophies at the Jet Propulsion Laboratory (JPL) during the past 25 years is presented. Examples from the JPL's Viking, Voyager and Galileo spacecraft are used to explain the changes in philosophy necessary to meet the program requirements with a reduction in cost and schedule. Approaches to validate mathematical models of large structures which can't be ground tested as an overall system because of size and/or adverse effects of terrestrial conditions such as gravity are presented.
Spacecraft load, design and test philosophies
1986-04-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Apollo Spacecraft Propulsion Systems Design Philosophies
British Library Conference Proceedings | 2010
|APOLLO SPACECRAFT PROPULSION SYSTEMS DESIGN PHILOSOPHIES
AIAA | 2010
|Online Contents | 1996
Test Philosophies for the New Millennium
British Library Conference Proceedings | 1996
|