The development of force and acceleration control spectra for vibration testing of Space Shuttle (STS) orbiter sidewall-mounted payloads requiresreliable estimates of the sidewall apparent weight and free (i.e. unloaded) vibration during lift-off. The feasibility of analytically predicting these quantities has been investigated through the development and analysis of a finite element model of the STS cargo bay. Analytical predictions of the sidewall apparent weight were compared with apparent weight measurements made on OV-101, and analytical predictions of the sidewall free vibration response during lift-off were compared with flight measurements obtained from STS-3 and STS-4. These analysis suggest that the cargo bay finite element model has potential application for the estimation of force and acceleration control spectra for STS sidewall-mounted payloads.
Prediction of force and acceleration control spectra for Space Shuttle orbiter sidewall-mounted payloads
Aerospace Testing Seminar ; 1990 ; Manhattan Beach, CA, United States
01.01.1990
Aufsatz (Konferenz)
Keine Angabe
Englisch
Orbiter ECLSS support of Shuttle payloads
NTRS | 1974
|Orbiter ECLSS support of shuttle payloads
Tema Archiv | 1974
|