Subsonic Aerodynamic Characteristics of a Proposed Advanced Manned Launch System Orbiter Configuration

Subsonic Aerodynamic Characteristics of a Proposed Advanced Manned Launch System Orbiter Configuration PDF Author: George M. Ware
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 36

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Subsonic Aerodynamic Characteristics of a Proposed Advanced Manned Launch System Orbiter Configuration

Subsonic Aerodynamic Characteristics of a Proposed Advanced Manned Launch System Orbiter Configuration PDF Author: George M. Ware
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 36

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Subsonic Aerodynamic Characteristics of a Proposed Advanced Manned Launch System Orbiter Configuration

Subsonic Aerodynamic Characteristics of a Proposed Advanced Manned Launch System Orbiter Configuration PDF Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781728672915
Category : Science
Languages : en
Pages : 34

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The Advanced Manned Launch System is a proposed near-term technology, two-stage, fully reusable launch system that consists of an unmanned glide-back booster and a manned orbiter. An orbiter model that featured a large fuselage and an aft delta wing with tip fins was tested in the Langley 7- by 10-Foot High-Speed Tunnel. A crew cabin, large payload fairing, and crew access tunnel were mounted on the upper body. The results of the investigation indicated that the configuration was longitudinally stable to an angle of attack of about 6 deg about a center-of-gravity position of 0.7 body length. The model had an untrimmed lift-drag ratio of 6.6, but could not be trimmed at positive lift. The orbiter model was also directionally unstable. The payload fairing was responsible for about half the instability. The tip-fin controllers, which are designed as active controls to produce artificial directional stability, were effective in producing yawing moment, but sizable adverse rolling moment occurred at angles of attack above 6 deg. Differential deflection of the elevon surfaces was effective in producing rolling moment with only small values of adverse yawing moment. Ware, George M. and Fox, Charles H., Jr. Langley Research Center RTOP 506-40-61-01

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 892

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AIAA/AHS/ASEE Aerospace Design Conference: 93-1001 - 93-1049

AIAA/AHS/ASEE Aerospace Design Conference: 93-1001 - 93-1049 PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 516

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Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
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Category : Government publications
Languages : en
Pages : 1786

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
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Category : Government publications
Languages : en
Pages :

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Monthly Catalog of United States Government Publications, Cumulative Index

Monthly Catalog of United States Government Publications, Cumulative Index PDF Author: United States. Superintendent of Documents
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Category : United States
Languages : en
Pages : 1466

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Research in Aeronautics and Space

Research in Aeronautics and Space PDF Author: Langley Research Center
Publisher:
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Category : Aeronautics
Languages : en
Pages : 380

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Government Reports Annual Index

Government Reports Annual Index PDF Author:
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Category : Government reports announcements & index
Languages : en
Pages : 1836

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Government Reports Announcements & Index

Government Reports Announcements & Index PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1506

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