Design, Fabrication and Test of a Formation of Two Satellites Connected by a Tether

Abstract

MR and MRS SAT are now in the flight vehicle construction/integration/test phase. Constraints have been clearly defined for each subsystem and efforts have shifted to integrated component testing. Subsystem timelines have been formed and are integrated in

Department(s)

Mechanical and Aerospace Engineering

Keywords and Phrases

Artificial Satellites; Formation Flight; Integration; Production; Radio Links; Satellite Pairs; Spacecraft Components; Wireless Communication

Document Type

Technical Report

Document Version

Citation

File Type

text

Language(s)

English

Rights

© 2007 University of Missouri--Rolla, All rights reserved.

Publication Date

01 Jan 2007

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