The results of a Phase 3 study of two Selected Tether Applications in Space (STAIS); deorbit of a Shuttle and launch of an Orbital Transfer Vehicle (OTV), both from the space station using a tether were examined. The study objectives were to: perform a preliminary engineering design, define operational scenarios, develop a common cost model, perform cost benefits analyses, and develop a Work Breakdown Structure (WBS). Key features of the performance analysis were to identify the net increases in effective Shuttle cargo capability if tethers are used to assist in the deorbit of Shuttles and the launching of the OTVs from the space station and to define deployer system designs required to accomplish these tasks. Deployer concepts were designe...
The first assessment is made of the design requirements and conceptual definition of a front end kit...
The mission and system requirements for the concept definition and system analysis of the Orbital Tr...
A Manned Mars Mission (M3) design study is proposed. The purpose of M3 is to transport 10 personnel ...
The major objective of the STS Propellant Scavenging Study is to define the hardware, operations, an...
Small Applications Technology Satellite program for developing sensors, experiments, and spacecraft ...
An operational Tether Deployment Monitoring System (TEDEMS) was constructed that would show system f...
A set of construction and assembly tasks required on the lunar surface was developed, different conc...
Propulsion system requirements to support Low Earth Orbit (LEO) manned space station development and...
Technologies for EVA and remote manipulation systems - handbook for systems designer
Conceptual design study of advanced Mariner space probe - flyby bus design for Mars missio
Volume 1 of the Final Study Report provides an Executive Summary of the Phase B study effort conduct...
The purpose of the Reusable Reentry Satellite (RRS) Propulsion System Trade Study described in this ...
The techniques required to produce and validate six detailed task timeline scenarios for crew worklo...
Applications for large deployable antennas were re-examined, flight demonstration objectives were de...
Feasibility of performing 1969 Mars Orbiter mission using Atlas Centaur launching vehicle - engineer...
The first assessment is made of the design requirements and conceptual definition of a front end kit...
The mission and system requirements for the concept definition and system analysis of the Orbital Tr...
A Manned Mars Mission (M3) design study is proposed. The purpose of M3 is to transport 10 personnel ...
The major objective of the STS Propellant Scavenging Study is to define the hardware, operations, an...
Small Applications Technology Satellite program for developing sensors, experiments, and spacecraft ...
An operational Tether Deployment Monitoring System (TEDEMS) was constructed that would show system f...
A set of construction and assembly tasks required on the lunar surface was developed, different conc...
Propulsion system requirements to support Low Earth Orbit (LEO) manned space station development and...
Technologies for EVA and remote manipulation systems - handbook for systems designer
Conceptual design study of advanced Mariner space probe - flyby bus design for Mars missio
Volume 1 of the Final Study Report provides an Executive Summary of the Phase B study effort conduct...
The purpose of the Reusable Reentry Satellite (RRS) Propulsion System Trade Study described in this ...
The techniques required to produce and validate six detailed task timeline scenarios for crew worklo...
Applications for large deployable antennas were re-examined, flight demonstration objectives were de...
Feasibility of performing 1969 Mars Orbiter mission using Atlas Centaur launching vehicle - engineer...
The first assessment is made of the design requirements and conceptual definition of a front end kit...
The mission and system requirements for the concept definition and system analysis of the Orbital Tr...
A Manned Mars Mission (M3) design study is proposed. The purpose of M3 is to transport 10 personnel ...