The platform payload accommodations, configuration drivers, and power system are described in detail. The platform design was analyzed and is presented. Demonstration tests are described and the results are reported
System concepts were characterized in order to define cost versus benefits for autonomous functional...
This is Volume 2 (Technical Report) of the Ford Aerospace & Communications Corporation Final Report ...
The capability of present technology and the Tracking and Data Relay Satellite System (TDRSS) to acc...
The system design philosphy applied in the development of this platform concept is summarized. The s...
The modularity, shape, and size of the recommended platform concept offers a low investment, early o...
Near term, cost effective concepts were defined to augment the power and duration capability offered...
Current and past space platform and power module studies were utilized to point the way to areas of ...
Electrical, mechanical, and software subsystem needs in the Post 1990 space operations environment a...
A study was conducted to derive and collect payload information on the anticipated space processing ...
Efforts are in progress to define an approach to provide a simple and cost effective solution to the...
The specific objectives of the study were to: (1) identify a viable conceptual design for the servic...
Design evolution, test article design, test article mass properties, and structural analysis of depl...
Program options are defined and requirements are determined for integrating crew, mass, volume, and ...
The top level system requirements are summarized and the accompanying conceptual design for an engin...
Examination of commercial equipment technologies revealed that the functional performance requiremen...
System concepts were characterized in order to define cost versus benefits for autonomous functional...
This is Volume 2 (Technical Report) of the Ford Aerospace & Communications Corporation Final Report ...
The capability of present technology and the Tracking and Data Relay Satellite System (TDRSS) to acc...
The system design philosphy applied in the development of this platform concept is summarized. The s...
The modularity, shape, and size of the recommended platform concept offers a low investment, early o...
Near term, cost effective concepts were defined to augment the power and duration capability offered...
Current and past space platform and power module studies were utilized to point the way to areas of ...
Electrical, mechanical, and software subsystem needs in the Post 1990 space operations environment a...
A study was conducted to derive and collect payload information on the anticipated space processing ...
Efforts are in progress to define an approach to provide a simple and cost effective solution to the...
The specific objectives of the study were to: (1) identify a viable conceptual design for the servic...
Design evolution, test article design, test article mass properties, and structural analysis of depl...
Program options are defined and requirements are determined for integrating crew, mass, volume, and ...
The top level system requirements are summarized and the accompanying conceptual design for an engin...
Examination of commercial equipment technologies revealed that the functional performance requiremen...
System concepts were characterized in order to define cost versus benefits for autonomous functional...
This is Volume 2 (Technical Report) of the Ford Aerospace & Communications Corporation Final Report ...
The capability of present technology and the Tracking and Data Relay Satellite System (TDRSS) to acc...