Hubble Space Telescope solar array change-out, mission anomalies and returned flight hardware

1994 ◽  
Author(s):  
Cindy Winslow
Keyword(s):  
Hubble Space Telescope ◽  
Solar Array ◽  
Space Telescope ◽  
Flight Hardware

Flight hardware for the Hubble Space Telescope solar array damper

2000 ◽  
Author(s):  
Joseph R. Maly ◽  
Satya M. Anandakrishnan ◽  
Scott C. Pendleton ◽  
E. Shade ◽  
J. W. Sills, Jr.
Keyword(s):  
Hubble Space Telescope ◽  
Solar Array ◽  
Space Telescope ◽  
Flight Hardware

scholarly journals Solar-array-induced disturbance of the Hubble Space Telescope pointing system

1995 ◽  
Vol 32 (4) ◽  
pp. 634-644 ◽  
Author(s):  
Carlton L. Foster ◽  
Michael L. Tinker ◽  
Gerald S. Nurre ◽  
William A. Till
Keyword(s):  
Hubble Space Telescope ◽  
Solar Array ◽  
Space Telescope

Solar Effects on Tensile and Optical Properties of Hubble Space Telescope Silver-Teflon Insulation

2006 ◽  
Vol 929 ◽  
Author(s):  
Kim K. de Groh ◽  
Joyce A. Dever ◽  
Aaron Snyder ◽  
Sharon Kaminski ◽  
Catherine E. McCarthy ◽  
...  
Keyword(s):  
Radiation Effects ◽  
Hubble Space Telescope ◽  
Strong Dependence ◽  
Thermal Control ◽  
Space Environment ◽  
Solar Array ◽  
Solar Absorptance ◽  
Space Telescope ◽  
Solar Arrays ◽  
Solar Exposure

ABSTRACTDuring the fourth servicing mission of the Hubble Space Telescope (HST), the second set of solar arrays (SA-II) was replaced with a third set and the SA-II was brought back to Earth. A section of the retrieved SA-II solar array drive arm (SADA) multilayer insulation (MLI), which experienced 8.25 years of space exposure, was provided to NASA Glenn Research Center for environmental durability analyses of the top layer of silver-Teflon fluorinated ethylene propylene (Ag-FEP). Because the SADA MLI had solar and anti-solar facing surfaces and was exposed to the space environment for a long duration, it provided a unique opportunity to study solar effects on environmental degradation of Ag-FEP, a commonly used spacecraft thermal control material. Therefore, the objective of this research was to characterize the degradation of retrieved HST SADA Ag-FEP with particular emphasis on solar radiation effects. Data obtained included tensile properties, solar absorptance, surface morphology and chemistry. The solar facing surface of the SADA was found to be extremely embrittled and contained numerous through-thickness cracks. Tensile testing indicated that the solar facing surface lost 60% of its mechanical strength and 90% of its elasticity while the anti-solar facing surface had ductility similar to pristine FEP. The solar absorptance of both the solar facing surface (0.155 ± 0.032) and the anti-solar facing surface (0.208 ± 0.012) were found to be greater than pristine Ag-FEP (0.074). Solar facing and anti-solar facing surfaces were microscopically textured, and locations of isolated contamination were present on the anti-solar surface resulting in increased localized texturing. Yet, the overall texture was significantly more pronounced on the solar facing surface indicating a synergistic effect of combined solar exposure and increased heating with atomic oxygen erosion. The results indicate a very strong dependence of degradation, particularly embrittlement, upon solar exposure with orbital thermal cycling having a significant effect.

The flight hardware and ground system for Hubble Space Telescope astrometry

1991 ◽  
Vol 103 ◽  
pp. 317 ◽  
Author(s):  
A. Bradley ◽  
L. Abramowicz-Reed ◽  
D. Story ◽  
G. Benedict ◽  
W. Jefferys
Keyword(s):  
Hubble Space Telescope ◽  
Space Telescope ◽  
Ground System ◽  
Flight Hardware

Torsional Buckling of the Hubble Space Telescope Solar Arrays

1998 ◽  
Vol 13 (2) ◽  
pp. 65-74
Author(s):  
Earl A. Thornton ◽  
David L Eby ◽  
Peter W. Chung
Keyword(s):  
Cross Section ◽  
Hubble Space Telescope ◽  
Solar Array ◽  
Torsional Buckling ◽  
Buckling Loads ◽  
Space Telescope ◽  
Linear Elastic ◽  
Solar Arrays ◽  
Buckling Behavior ◽  
Open Cross Section

The buckling behavior of a flexible rolled-up solar array used on the Hubble Space Telescope (HST) is investigated analytically and experimentally. Analytically, the solar array is modeled assuming the booms are linear, elastic beams of open cross-section, and the solar blanket is represented as an inextensible membrane. The analyses determine critical buckling loads for flexure and torsion. The behavior of the solar array is also investigated by experiments conducted using a model solar array with (1) closed cross-section booms, and (2) tubular booms like those used on the HST. The analyses and experiments show that the Hubble's solar arrays were deployed with a preload that caused them to buckle in torsion. Based on the study, an hypothesis is suggested for the failure of the solar array's booms that was discovered by the astronauts in 1993.

scholarly journals Microparticle Impacts Observed on the Hubble Space Telescope Solar Array

1996 ◽  
Vol 150 ◽  
pp. 213-216
Author(s):  
Lucinda Berthoud ◽  
Klaus Paul
Keyword(s):  
Hubble Space Telescope ◽  
Low Earth Orbit ◽  
Solar Array ◽  
Earth Orbit ◽  
Space Telescope ◽  
High Orbit

AbstractThe recent recovery of the Hubble Space Telescope (HST) Solar-Array-1 offers a unique opportunity to improve our knowledge of the low Earth orbit (LEO) particle environment. The data from HST surfaces is particularly interesting for the meteoroid and debris community, as the Telescope was in orbit at an altitude of approximately 614 km and there has been no data from such a high orbit before.

Sign in / Sign up

Export Citation Format

Share Document