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Thruster configurations for maneuvering heavy payloadsThe Cargo Transfer Vehicle (CTV) will be required to perform six degree of freedom (6 DOF) maneuvers while carrying a wide range of payloads varying from 100,000 lbm to no payload. The current baseline design configuration for the CTV uses a forward propulsion module (FPM) mounted in front of the payload with the CTV behind the payload so that the center of gravity (CG) of the combined stack is centered between the thruster sets. This allows for efficient rotations and translations of heavy payloads in all directions; however, the FPM is a costly item, so it is desirable to find design solutions that do not require the FPM. This presentation provides an overview of the analysis of the FPM requirements for the CTV. In this study, only the reaction control system (RCS) thruster configurations are considered for 6 DOF maneuvers of various CTV cargo configurations. An important output of this study are the viable alternative thruster configurations that eliminate the need for the FPM. Initial results were derived using analytical techniques and simulation analysis tools. Results from the preliminary analysis were validated using our 6 DOF simulation.
Document ID
19930012226
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tsugawa, Roy K.
(TRW, Inc. Redondo Beach, CA., United States)
Draznin, Michael E.
(TRW, Inc. Redondo Beach, CA., United States)
Dabney, Richard W.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Publication Information
Publication: NASA, Washington, NASA Automated Rendezvous and Capture Review. Executive Summary
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
93N21415
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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