A quantitative cost for various Spacelab flight hardware configurations is provided along with varied software development options. A cost analysis of Spacelab computer hardware and software is presented. The cost study is discussed based on utilization of a central experiment computer with optional auxillary equipment. Groundrules and assumptions used in deriving the costing methods for all options in the Spacelab experiment study are presented. The groundrules and assumptions, are analysed and the options along with their cost considerations, are discussed. It is concluded that Spacelab program cost for software development and maintenance is independent of experimental hardware and software options, that distributed standard computer con...
The feasibility and cost savings of using flight-proven components in designing spacecraft were inve...
The recent successful flight of Spacelab 1 while being the culmination of over 10 years of internati...
The main characteristics of the Spacelab system are described. Sufficient information on Spacelab ca...
The primary objective of this study was to develop an integrated approach for the development, imple...
The total matrix of alternate Spacelab processing concepts and the rejection rationale utilized to r...
The integration and checkout activities of Spacelab payloads consist of two major sets of tasks: su...
A study was conducted to define the complexity and magnitude of the Spacelab software challenge. The...
The engineering analyses and evaluation studies conducted for the Software Requirements Analysis are...
The capital investment for the integration and checkout of Spacelab payloads is assessed. Detailed d...
An overview of the study is presented. A synopsis of processing concepts for the Spacelab configurat...
A detailed analysis is presented of each selected equipment item, and suitability and cost analyses ...
The resources requirements for the integration and checkout of spacelab payloads are presented in th...
Cost effective techniques for addressing management and operational activities on Spacelab were iden...
Alternate level 4 integration approaches were synthesized and evaluated to establish the most cost e...
Cost estimates for experiments and subsystems flown in the Spacelab were established. Ten experiment...
The feasibility and cost savings of using flight-proven components in designing spacecraft were inve...
The recent successful flight of Spacelab 1 while being the culmination of over 10 years of internati...
The main characteristics of the Spacelab system are described. Sufficient information on Spacelab ca...
The primary objective of this study was to develop an integrated approach for the development, imple...
The total matrix of alternate Spacelab processing concepts and the rejection rationale utilized to r...
The integration and checkout activities of Spacelab payloads consist of two major sets of tasks: su...
A study was conducted to define the complexity and magnitude of the Spacelab software challenge. The...
The engineering analyses and evaluation studies conducted for the Software Requirements Analysis are...
The capital investment for the integration and checkout of Spacelab payloads is assessed. Detailed d...
An overview of the study is presented. A synopsis of processing concepts for the Spacelab configurat...
A detailed analysis is presented of each selected equipment item, and suitability and cost analyses ...
The resources requirements for the integration and checkout of spacelab payloads are presented in th...
Cost effective techniques for addressing management and operational activities on Spacelab were iden...
Alternate level 4 integration approaches were synthesized and evaluated to establish the most cost e...
Cost estimates for experiments and subsystems flown in the Spacelab were established. Ten experiment...
The feasibility and cost savings of using flight-proven components in designing spacecraft were inve...
The recent successful flight of Spacelab 1 while being the culmination of over 10 years of internati...
The main characteristics of the Spacelab system are described. Sufficient information on Spacelab ca...