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 Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722826314
Category :
Languages : en
Pages : 32

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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...

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 :
Languages : en
Pages : 27

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Aerodynamic Predictions and Experimental Results for an Advanced Manned Launch System Orbiter Configuration

Aerodynamic Predictions and Experimental Results for an Advanced Manned Launch System Orbiter Configuration PDF Author: Walter C. Engelund
Publisher:
ISBN:
Category :
Languages : en
Pages :

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Subsonic Aerodynamic Characteristics of the HL-20 Lifting-body Configuration

Subsonic Aerodynamic Characteristics of the HL-20 Lifting-body Configuration PDF Author: George M. Ware
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 36

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Influence of Configuration Details on the Subsonic Characteristics of a Space Shuttle Orbiter Design

Influence of Configuration Details on the Subsonic Characteristics of a Space Shuttle Orbiter Design PDF Author: John P. Decker
Publisher:
ISBN:
Category : Space shuttles
Languages : en
Pages : 40

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Scientific and Technical Aerospace Reports

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

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Low Subsonic Aerodynamic Characteristics of a Shuttle Orbiter Configuration Designed for Reduced Length

Low Subsonic Aerodynamic Characteristics of a Shuttle Orbiter Configuration Designed for Reduced Length PDF Author: George M. Ware
Publisher:
ISBN:
Category :
Languages : en
Pages : 38

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Effect of Configuration Modifications on the Low-subsonic Aerodynamic Characteristics of a Space Shuttle-orbiter Concept with a Blended Delta Wing-body

Effect of Configuration Modifications on the Low-subsonic Aerodynamic Characteristics of a Space Shuttle-orbiter Concept with a Blended Delta Wing-body PDF Author: Delma C. Jr Freeman
Publisher:
ISBN:
Category :
Languages : en
Pages : 61

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Subsonic Aerodynamic Characteristics of a Space Shuttle Orbiter

Subsonic Aerodynamic Characteristics of a Space Shuttle Orbiter PDF Author: James C. Ellison
Publisher:
ISBN:
Category :
Languages : en
Pages : 24

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