The major objective of the STS Propellant Scavenging Study is to define the hardware, operations, and life cycle costs for recovery of unused Space Transportation System propellants. Earlier phases were concerned exclusively with the recovery of cryogenic propellants from the main propulsion system of the manned STS. The phase of the study covered by this report (Part II Extension) modified the objectives to include cryogenic propellants delivered to orbit by the unmanned cargo vehicle. The Part II Extension had the following objectives: (1) predict OTV propellant requirements from 1995 to 2010; investigate scavenging/transport tank reuse; determine optimum tank sizing and arrangement; and develop hardware concepts for tanks
The LAWS phase 1 and phase 2 studies have been completed on schedule and have led to significant adv...
Conceptual design study of advanced Mariner space probe - Mars lander configuratio
A preliminary design of a two-stage to orbit vehicle was conducted with the requirements to carry a ...
Technologies for EVA and remote manipulation systems - handbook for systems designer
Prototype space flight experiment package for study of circadian periodicity in pocket mic
Conceptual design study of advanced Mariner space probe - flyby bus design for Mars missio
Technology was identified which will enable application of hybrid propulsion to manned and unmanned ...
The purpose of the Reusable Reentry Satellite (RRS) Propulsion System Trade Study described in this ...
Propulsion system requirements to support Low Earth Orbit (LEO) manned space station development and...
Techniques for orbital refueling of space based vehicles were developed and experimental programs to...
The results of a Phase 3 study of two Selected Tether Applications in Space (STAIS); deorbit of a Sh...
Applications for large deployable antennas were re-examined, flight demonstration objectives were de...
The program objectives of developing hybrid propulsion technology (HPT) to enable its application fo...
An improved understanding of low gravity subcritical cryogenic fluid behavior is critical for the co...
Data processing system and flight evaluation plan for gravity gradient stabilization system for Appl...
The LAWS phase 1 and phase 2 studies have been completed on schedule and have led to significant adv...
Conceptual design study of advanced Mariner space probe - Mars lander configuratio
A preliminary design of a two-stage to orbit vehicle was conducted with the requirements to carry a ...
Technologies for EVA and remote manipulation systems - handbook for systems designer
Prototype space flight experiment package for study of circadian periodicity in pocket mic
Conceptual design study of advanced Mariner space probe - flyby bus design for Mars missio
Technology was identified which will enable application of hybrid propulsion to manned and unmanned ...
The purpose of the Reusable Reentry Satellite (RRS) Propulsion System Trade Study described in this ...
Propulsion system requirements to support Low Earth Orbit (LEO) manned space station development and...
Techniques for orbital refueling of space based vehicles were developed and experimental programs to...
The results of a Phase 3 study of two Selected Tether Applications in Space (STAIS); deorbit of a Sh...
Applications for large deployable antennas were re-examined, flight demonstration objectives were de...
The program objectives of developing hybrid propulsion technology (HPT) to enable its application fo...
An improved understanding of low gravity subcritical cryogenic fluid behavior is critical for the co...
Data processing system and flight evaluation plan for gravity gradient stabilization system for Appl...
The LAWS phase 1 and phase 2 studies have been completed on schedule and have led to significant adv...
Conceptual design study of advanced Mariner space probe - Mars lander configuratio
A preliminary design of a two-stage to orbit vehicle was conducted with the requirements to carry a ...