Add to ORKGMission requirements and physical and functional characteristics for optimized cost orbital space transportation system desig
Normal technology requirements applicable to Single Stage to Orbit (SSTO) systems were projected to ...
Program options are defined and requirements are determined for integrating crew, mass, volume, and ...
The platform payload accommodations, configuration drivers, and power system are described in detail...
Plans, schedules, and operations and support data for optimized cost orbital space transportation sy...
A methodology for developing balanced designs of spacecraft subsystems which interrelates cost, perf...
A methodology which was developed for balanced designing of spacecraft subsystems and interrelates c...
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 ...
The relationships between performance, safety, cost, and schedule parameters were identified and qua...
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...
Specific system options are defined and identified for a cost effective space station capable of ord...
Program development, cost analysis, and technology requirements for reusable space shuttle systems h...
The results of a space station conceptual design and evaluation study are summarized. The study repr...
Mass properties data for two stage fixed wing reusable space transportation system - Vol.
Normal technology requirements applicable to Single Stage to Orbit (SSTO) systems were projected to ...
Program options are defined and requirements are determined for integrating crew, mass, volume, and ...
The platform payload accommodations, configuration drivers, and power system are described in detail...
Plans, schedules, and operations and support data for optimized cost orbital space transportation sy...
A methodology for developing balanced designs of spacecraft subsystems which interrelates cost, perf...
A methodology which was developed for balanced designing of spacecraft subsystems and interrelates c...
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 ...
The relationships between performance, safety, cost, and schedule parameters were identified and qua...
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...
Specific system options are defined and identified for a cost effective space station capable of ord...
Program development, cost analysis, and technology requirements for reusable space shuttle systems h...
The results of a space station conceptual design and evaluation study are summarized. The study repr...
Mass properties data for two stage fixed wing reusable space transportation system - Vol.
Normal technology requirements applicable to Single Stage to Orbit (SSTO) systems were projected to ...
Program options are defined and requirements are determined for integrating crew, mass, volume, and ...
The platform payload accommodations, configuration drivers, and power system are described in detail...