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Multi-Axis Transient Testing "Final Report".

Eckhardt, K.(1) and Hüners, H. and Schmidt, G.(2) (1990) Multi-Axis Transient Testing "Final Report". Project Report, DLR-Interner Bericht. ESTEC Contract No. 6558/85/NL/PH, 73 S.

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Abstract

The aim of "multi-axis transient testing" is the correct stress distributed loading of spacecraft structure hardware. Following this test approach, further practical experiences are available demonstrating the ability to simulate actual load environment. This report presents test results from a pilot facility at HRB, Juelich, achieved with a redundantly suspended Spacelab Pallet Structural Model. The results are compared with presently existing requirements for a future facility for spacecraft transient testing. The identified development areas are discussed and possible improvements are listed.

Document Type:Monograph (Project Report, DLR-Interner Bericht)
Additional Information: LIDO-Berichtsjahr=1990,
Title:Multi-Axis Transient Testing "Final Report".
Authors:
AuthorsInstitution or Email of Authors
Eckhardt, K.(1)UNSPECIFIED
Hüners, H.UNSPECIFIED
Schmidt, G.(2)UNSPECIFIED
Date:1990
Journal or Publication Title:ESTEC Contract No. 6558/85/NL/PH
Number of Pages:73
Status:Published
Keywords:Transient Testing, Dynamic Qualification, Hydraulic Vibration, Interf ace Excitation
Institution:MBB/ERNO
HGF - Research field:UNSPECIFIED
HGF - Program:other
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:no assignment
DLR - Research theme (Project):UNSPECIFIED
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity
Deposited By: elib DLR-Beauftragter
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 10:41

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