Add to ORKGThe feasibility and cost savings of using flight-proven components in designing spacecraft were investigated. The components analyzed were (1) large space telescope, (2) stratospheric aerosol and gas equipment, (3) mapping mission, (4) solar maximum mission, and (5) Tiros-N. It is concluded that flight-proven hardware can be used with not-too-extensive modification, and significant savings can be realized. The cost savings for each component are presented
Payloads to be launched on the space shuttle/space tug/sortie lab combinations are discussed. The pa...
Near term, cost effective concepts were defined to augment the power and duration capability offered...
The Satellite Telecommunications Analysis and Modeling Program (STAMP) provides the user with a flex...
The program procedures that were incorporated into an on-going "design-to-cost" spacecraft program a...
A methodology for developing balanced designs of spacecraft subsystems which interrelates cost, perf...
A detailed analysis is presented of each selected equipment item, and suitability and cost analyses ...
A study is described which was initiated to identify and quantify the interrelationships between and...
The systems cost/performance model was implemented as a digital computer program to perform initial ...
A preliminary technical and economic feasibility study was made of the use of Standardized Interstat...
A study of the comparative program costs associated with use of various standardized spacecraft for ...
Man's contribution to the achievement of scientific mission objectives in the space environment is i...
The relationships between performance, safety, cost, and schedule parameters were identified and qua...
A recommended baseline system is presented along with alternate avionics systems, Mark 2 avionics, b...
A methodology which was developed for balanced designing of spacecraft subsystems and interrelates c...
Examination of commercial equipment technologies revealed that the functional performance requiremen...
Payloads to be launched on the space shuttle/space tug/sortie lab combinations are discussed. The pa...
Near term, cost effective concepts were defined to augment the power and duration capability offered...
The Satellite Telecommunications Analysis and Modeling Program (STAMP) provides the user with a flex...
The program procedures that were incorporated into an on-going "design-to-cost" spacecraft program a...
A methodology for developing balanced designs of spacecraft subsystems which interrelates cost, perf...
A detailed analysis is presented of each selected equipment item, and suitability and cost analyses ...
A study is described which was initiated to identify and quantify the interrelationships between and...
The systems cost/performance model was implemented as a digital computer program to perform initial ...
A preliminary technical and economic feasibility study was made of the use of Standardized Interstat...
A study of the comparative program costs associated with use of various standardized spacecraft for ...
Man's contribution to the achievement of scientific mission objectives in the space environment is i...
The relationships between performance, safety, cost, and schedule parameters were identified and qua...
A recommended baseline system is presented along with alternate avionics systems, Mark 2 avionics, b...
A methodology which was developed for balanced designing of spacecraft subsystems and interrelates c...
Examination of commercial equipment technologies revealed that the functional performance requiremen...
Payloads to be launched on the space shuttle/space tug/sortie lab combinations are discussed. The pa...
Near term, cost effective concepts were defined to augment the power and duration capability offered...
The Satellite Telecommunications Analysis and Modeling Program (STAMP) provides the user with a flex...