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Volumn , Issue , 2001, Pages

Deployment repeatability of a space telescope reflector petal

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; DEGREES OF FREEDOM (MECHANICS); HYSTERESIS; SPACE TELESCOPES;

EID: 85067319841     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-1302     Document Type: Conference Paper
Times cited : (2)

References (12)
  • 2
    • 84894423089 scopus 로고    scopus 로고
    • . Composite Optics, Inc. "Deployable Lidar Telescope Development: Preliminary Design and Analysis (Work Units I-III), Final Report", SP- 1098-042098, April 17
    • Composite Optics, Inc. "Deployable Lidar Telescope Development: Preliminary Design and Analysis (Work Units I-III), Final Report", SP- 1098-042098, April 17, 1998.
    • (1998)
  • 9
    • 84894445324 scopus 로고    scopus 로고
    • "Next Generation Space Telescope Level 2 Requirements", NGST-REQT-000624, Goddard Space Flight Center, Greenbelt, MD, April
    • "Next Generation Space Telescope Level 2 Requirements", NGST-REQT-000624, Goddard Space Flight Center, Greenbelt, MD, April 2001.
    • (2001)
  • 12
    • 0033366246 scopus 로고    scopus 로고
    • Submicron mechanical stability of a prototype deployable space telescope support structure
    • Sept.-Oct
    • Warren, Peter A., Peterson, Lee D., and Hinkle, Jason D., "Submicron mechanical stability of a prototype deployable space telescope support structure", Journal of Spacecraft and Rockets, vol. 36, no. 5, Sept.-Oct, 1999, pp. 765-771.
    • (1999) Journal of Spacecraft and Rockets , vol.36 , Issue.5 , pp. 765-771
    • Warren, P.A.1    Peterson, L.D.2    Jason, H.D.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.