The objectives of this program are to provide a demonstration of hydrogen/oxygen propulsion technology readiness for the initial operational capability (IOC) space station application, specifically gaseous hydrogen/oxygen and warm hydrogen thruster concepts, and to establish a means for evolving from the IOC space station propulsion system (SSPS) to that required to support and interface with advanced station functions. These objectives were met by analytical studies and by furnishing a propulsion test bed to the Marshall Space Flight Center for testing
The development of the manned space station has necessitated the development of technology related t...
Prototype components fabrication and performance tests in development of hydrogen-oxygen auxiliary s...
The technical highlights and accomplishments made at NASA LeRC in the development of the Space Stati...
The progress on the Space Station Propulsion Technology Program is described. The objectives are to ...
Conceptual designs for O2/H2 chemical and resistojet propulsion systems for the space station was de...
Two propulsion systems have been selected for the space station: O/H rockets for high thrust applica...
The completion of the Space Station Propulsion Advanced Technology Programs established an in-depth ...
A reference configuration was established for the initial operating capability (IOC) station. The re...
Viewgraphs on propulsion technology discipline for Space Station Freedom are presented. Topics cover...
The topics presented are covered in viewgraph form. Focused program elements are: (1) transportation...
The purpose of the Advanced Development program was to investigate propulsion options for the space ...
The topics covered include the following: (1) the next manned space transportation system; (2) devel...
A survey is provided of hydrogen/oxygen (H/O) auxiliary propulsion system (APS) concepts and low thr...
Two alternate oxygen-hydrogen auxiliary propulsion system concepts for use with the space shuttle ve...
A research and technology program for advanced high pressure, oxygen-hydrogen rocket propulsion tech...
The development of the manned space station has necessitated the development of technology related t...
Prototype components fabrication and performance tests in development of hydrogen-oxygen auxiliary s...
The technical highlights and accomplishments made at NASA LeRC in the development of the Space Stati...
The progress on the Space Station Propulsion Technology Program is described. The objectives are to ...
Conceptual designs for O2/H2 chemical and resistojet propulsion systems for the space station was de...
Two propulsion systems have been selected for the space station: O/H rockets for high thrust applica...
The completion of the Space Station Propulsion Advanced Technology Programs established an in-depth ...
A reference configuration was established for the initial operating capability (IOC) station. The re...
Viewgraphs on propulsion technology discipline for Space Station Freedom are presented. Topics cover...
The topics presented are covered in viewgraph form. Focused program elements are: (1) transportation...
The purpose of the Advanced Development program was to investigate propulsion options for the space ...
The topics covered include the following: (1) the next manned space transportation system; (2) devel...
A survey is provided of hydrogen/oxygen (H/O) auxiliary propulsion system (APS) concepts and low thr...
Two alternate oxygen-hydrogen auxiliary propulsion system concepts for use with the space shuttle ve...
A research and technology program for advanced high pressure, oxygen-hydrogen rocket propulsion tech...
The development of the manned space station has necessitated the development of technology related t...
Prototype components fabrication and performance tests in development of hydrogen-oxygen auxiliary s...
The technical highlights and accomplishments made at NASA LeRC in the development of the Space Stati...