Thermal distortion of over 10 Meter diameter reflectors formed by truss structure

Akihiro Miyasaka, Jin Mitsugi

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

This paper describes how an on-board satellite large reflector structure was designed based on the thermal distortion predicted by structural analysis in coordination with thermal estimation. As the reflector consists of many small similar modules, it is possible to simplify the analytical model and the fabrication process. Module size and number are decided by estimating the surface accuracy for a 13 m aperture reflector. The maximum thermal distortion is found to be occurred during eclipses. As the module number increases, the thermal distortion increases. When the antenna system is used in 2.5. G Hz (S frequency bands), total surface accuracy needs to be 2.4 mm RMS (specified value). This requirement is satisfied by a reflector composed of 14 modules; maximum error is 1.6 mm RMS by slight repositioning the reflector.

Original languageEnglish
Title of host publication32nd Thermophysics Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9780000000002
Publication statusPublished - 1997
Externally publishedYes
Event32nd Thermophysics Conference, 1997 - Atlanta, United States
Duration: 1997 Jun 231997 Jun 25

Other

Other32nd Thermophysics Conference, 1997
CountryUnited States
CityAtlanta
Period97/6/2397/6/25

Fingerprint

reflectors
modules
Structural analysis
Frequency bands
eclipses
Analytical models
structural analysis
Satellites
Antennas
Fabrication
estimating
antennas
apertures
Hot Temperature
requirements
fabrication

ASJC Scopus subject areas

  • Mechanical Engineering
  • Aerospace Engineering
  • Condensed Matter Physics

Cite this

Miyasaka, A., & Mitsugi, J. (1997). Thermal distortion of over 10 Meter diameter reflectors formed by truss structure. In 32nd Thermophysics Conference [AIAA-97-2457] American Institute of Aeronautics and Astronautics Inc, AIAA.

Thermal distortion of over 10 Meter diameter reflectors formed by truss structure. / Miyasaka, Akihiro; Mitsugi, Jin.

32nd Thermophysics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, 1997. AIAA-97-2457.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Miyasaka, A & Mitsugi, J 1997, Thermal distortion of over 10 Meter diameter reflectors formed by truss structure. in 32nd Thermophysics Conference., AIAA-97-2457, American Institute of Aeronautics and Astronautics Inc, AIAA, 32nd Thermophysics Conference, 1997, Atlanta, United States, 97/6/23.
Miyasaka A, Mitsugi J. Thermal distortion of over 10 Meter diameter reflectors formed by truss structure. In 32nd Thermophysics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA. 1997. AIAA-97-2457
Miyasaka, Akihiro ; Mitsugi, Jin. / Thermal distortion of over 10 Meter diameter reflectors formed by truss structure. 32nd Thermophysics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, 1997.
@inproceedings{5f33074e81444fc39e098bcef3bf1aaf,
title = "Thermal distortion of over 10 Meter diameter reflectors formed by truss structure",
abstract = "This paper describes how an on-board satellite large reflector structure was designed based on the thermal distortion predicted by structural analysis in coordination with thermal estimation. As the reflector consists of many small similar modules, it is possible to simplify the analytical model and the fabrication process. Module size and number are decided by estimating the surface accuracy for a 13 m aperture reflector. The maximum thermal distortion is found to be occurred during eclipses. As the module number increases, the thermal distortion increases. When the antenna system is used in 2.5. G Hz (S frequency bands), total surface accuracy needs to be 2.4 mm RMS (specified value). This requirement is satisfied by a reflector composed of 14 modules; maximum error is 1.6 mm RMS by slight repositioning the reflector.",
author = "Akihiro Miyasaka and Jin Mitsugi",
year = "1997",
language = "English",
isbn = "9780000000002",
booktitle = "32nd Thermophysics Conference",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",

}

TY - GEN

T1 - Thermal distortion of over 10 Meter diameter reflectors formed by truss structure

AU - Miyasaka, Akihiro

AU - Mitsugi, Jin

PY - 1997

Y1 - 1997

N2 - This paper describes how an on-board satellite large reflector structure was designed based on the thermal distortion predicted by structural analysis in coordination with thermal estimation. As the reflector consists of many small similar modules, it is possible to simplify the analytical model and the fabrication process. Module size and number are decided by estimating the surface accuracy for a 13 m aperture reflector. The maximum thermal distortion is found to be occurred during eclipses. As the module number increases, the thermal distortion increases. When the antenna system is used in 2.5. G Hz (S frequency bands), total surface accuracy needs to be 2.4 mm RMS (specified value). This requirement is satisfied by a reflector composed of 14 modules; maximum error is 1.6 mm RMS by slight repositioning the reflector.

AB - This paper describes how an on-board satellite large reflector structure was designed based on the thermal distortion predicted by structural analysis in coordination with thermal estimation. As the reflector consists of many small similar modules, it is possible to simplify the analytical model and the fabrication process. Module size and number are decided by estimating the surface accuracy for a 13 m aperture reflector. The maximum thermal distortion is found to be occurred during eclipses. As the module number increases, the thermal distortion increases. When the antenna system is used in 2.5. G Hz (S frequency bands), total surface accuracy needs to be 2.4 mm RMS (specified value). This requirement is satisfied by a reflector composed of 14 modules; maximum error is 1.6 mm RMS by slight repositioning the reflector.

UR - http://www.scopus.com/inward/record.url?scp=84964009573&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=84964009573&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:84964009573

SN - 9780000000002

BT - 32nd Thermophysics Conference

PB - American Institute of Aeronautics and Astronautics Inc, AIAA

ER -