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A Shuttle Derived Vehicle Launch System Martin Marietta Aerospace Michoud Div. New Orleans, LA

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Tewell, J. Robert, author.
Conference Name:
Aerospace Congress & Exposition (1982-10-25 : Anaheim, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1982
Summary:
This paper describes a Shuttle Derived Vehicle (SDV) launch system presently being studied for the NASA by Martin Marietta Aerospace which capitalizes on existing Shuttle hardware elements to provide increased accommodations for payload weight, payload volume, or both.* The SDV configuration utilizes the existing solid rocket boosters, external tank and the space shuttle main engines but replaces the manned orbiter with an unmanned, remotely controlled cargo carrier. This cargo carrier substitution more than doubles the performance capability of the orbiter system and is realistically achievable for minimal cost. The advantages of the SDV are presented in terms of performance and economics. Based on these considerations, it is concluded that an unmanned SDV offers a most attractive complement to the present Space Transportation System
Notes:
Vendor supplied data
Publisher Number:
821342
Access Restriction:
Restricted for use by site license

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