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Review of Our National Heritage of Launch Vehicles Using Aerodynamic Surfaces and Current Use of These by Other Nations (Center Director's Discretionary Fund Project 93-05 Part II)

NASA/TR-3615, Barret , C., Review of Our National Heritage of Launch Vehicles Using Aerodynamic Surfaces and Current Use of These by Other Nations (Center Director's Discretionary Fund Project 93-05 Part II) , Structures and Dynamics Laboratory, Science and Engineering Directorate. NASA arshall Space Flight Center, AL 35812 , April 1996, pp. 69, Format(s): PDF 1495k

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Marshall Space Flight Center has a rich heritage of launch vehicles that have used aerodynamic surfaces for flight stability and for flight control. Recently, due to the aft center-of-gravity (cg) locations on launch vehicles currently being studied, the need has arisen for the vehicle control augmentation that can be provided by these flight controls. Aerodynamic flight control can also reduce engine gimbaling requirements, provide actuator failure protection, enhance crew safety, and increase vehicle reliability and payload capability. As a starting point for the novel design of aerodynamic flight control augmentors for a Saturn class, aft cg launch vehicle, this report undertakes a review of our national heritage of launch vehicles using aerodynamic surfaces, along with a survey of current use of aerodynamic surfaces on large launch vehicles of other nations. This report presents one facet of Center Director's Discretionary Fund Project 93-05 and has a previous and subsequent companion publication.
Keywords:launch vehicle flight control surfaces, launch vehicle aerodynamic surfaces, launch vehicle flight control augmentation, saturn i, saturn i-b, saturn v, x-15, foreign launch vehicle aerodynamic surfaces
CASI Document ID Number:96N26811
Subjects:Astronautics: Launch Vehicles And Launch Operations: Launch Vehicles
ID Code:321
Deposited On:01 July 2002