Multimission modular spacecraft (MMS)

Author:

FALKENHAYN, JR. EDWARD1

Affiliation:

1. NASA, Goddard Space Flight Center, Greenbelt, MD

Publisher

American Institute of Aeronautics and Astronautics

Reference8 articles.

1. In the mid 1970'5, NASA Headquarters authorized the GSFC to proceed with the full-scale development of the MMS. In the same time frame, the Solar Maximum Mission (SMM) received program go-ahead, and the decision was made that SMM would be the first customer of the MMS. Following SMM in short order, the MMS was selected for the earth resources, Landsat Observatories and then the Upper Atmosphere Research Satellite (UARS) . The comparative specifications for these three programs are presented on the chart below.

2. (LaunchConfiguration)

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1. MBSE Methods for Inheritance and Design Reuse;Handbook of Model-Based Systems Engineering;2023

2. MBSE Methods for Inheritance and Design Reuse;Handbook of Model-Based Systems Engineering;2023

3. Introduction;Fundamentals of Spacecraft Attitude Determination and Control;2014

4. Modular Thermal Control Architecture for Modular Spacecraft;49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference <br> 16th AIAA/ASME/AHS Adaptive Structures Conference<br> 10t;2008-04-07

5. On-board attitude determination for the Topex satellite;Guidance, Navigation and Control Conference;1989-08-14

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