Add to ORKGData on the performance, stability, and thermal characteristics of an OME operating with an alternate injector configuration and with alternate propellants was obtained. The design, manufacturing, and operating characteristics of an electroformed, regeneratively cooled thrust chamber were also derived. Subscale and full scale tests provide data relating to off-design and transient operation
NASA intends to pursue technology applications to upgrade the Space Shuttle Orbiter OMS and RCS syst...
Descriptions are given of the test hardware, facility, procedures, and results of electrically heate...
Preliminary design considerations and changes made in the baseline space shuttle orbital maneuvering...
Analyses and preliminary designs of candidate OME propellant combinations and corresponding engine d...
The characteristics and performance of the orbit maneuvering engine for the space shuttle are discus...
An analytical and design study was conducted to compare the high and low contraction ratio thrust ch...
The test program conducted to characterize the steady state stability, thermal, and performance char...
An evaluation of reusable thrust chambers for the space shuttle orbit maneuvering engine was conduct...
The stability characteristics of the like-doublet injector were defined over the range of OME chambe...
A subscale injector test program conducted with a ten-inch diameter like-doublet injector to determi...
Test hardware, facilities, and procedures are described along with results of electrically heated tu...
A platelet face injector for the Orbit Maneuvering Engine (OME) on the space shuttle was evaluated a...
The performance and heat transfer characteristics of a doublet element type injector for the space s...
An abbreviated program was conducted to investigate igniter, injector, and thrust chamber technology...
The current Space Shuttle Orbital Maneuvering Engine (OME) is pressure fed, utilizing storable prope...
NASA intends to pursue technology applications to upgrade the Space Shuttle Orbiter OMS and RCS syst...
Descriptions are given of the test hardware, facility, procedures, and results of electrically heate...
Preliminary design considerations and changes made in the baseline space shuttle orbital maneuvering...
Analyses and preliminary designs of candidate OME propellant combinations and corresponding engine d...
The characteristics and performance of the orbit maneuvering engine for the space shuttle are discus...
An analytical and design study was conducted to compare the high and low contraction ratio thrust ch...
The test program conducted to characterize the steady state stability, thermal, and performance char...
An evaluation of reusable thrust chambers for the space shuttle orbit maneuvering engine was conduct...
The stability characteristics of the like-doublet injector were defined over the range of OME chambe...
A subscale injector test program conducted with a ten-inch diameter like-doublet injector to determi...
Test hardware, facilities, and procedures are described along with results of electrically heated tu...
A platelet face injector for the Orbit Maneuvering Engine (OME) on the space shuttle was evaluated a...
The performance and heat transfer characteristics of a doublet element type injector for the space s...
An abbreviated program was conducted to investigate igniter, injector, and thrust chamber technology...
The current Space Shuttle Orbital Maneuvering Engine (OME) is pressure fed, utilizing storable prope...
NASA intends to pursue technology applications to upgrade the Space Shuttle Orbiter OMS and RCS syst...
Descriptions are given of the test hardware, facility, procedures, and results of electrically heate...
Preliminary design considerations and changes made in the baseline space shuttle orbital maneuvering...