scholarly journals The solid surface combustion Space Shuttle experiment hardware description and ground-based test results

Author(s):  
D. VENTO ◽  
R. ZAVESKY ◽  
K. SACKSTEDER ◽  
R. ALTENKIRCH
1974 ◽  
Vol 18 (2) ◽  
pp. 187-187
Author(s):  
A. M. Ray

A test bed type astronaut maneuvering unit was designed and evaluated with the assistance of Martin Marietta's six degree of freedom simulator. Four different control modes were developed for this unit for test and evaluation inside Skylab's 22 foot diameter orbital workshop. The orbital tests have provided the experience and technology base necessary for space Shuttle and space station astronaut maneuvering unit design requirements. This paper is an overview of the M509 experiment hardware, procedures, and results with emphasis on the comparison between on-orbit test results and the six degree of freedom simulator. The simulator was used to develop the unit's design requirements, evaluate the control logic parameters, and for developing maneuvers and training the crew. The simulator will also be flown by the Skylab crews in May for post flight evaluation and simulator calibration. (Films of the simulations and on-orbit flight are available as part of this presentation.)


1986 ◽  
Vol 87 ◽  
Author(s):  
Michael J. Martin

AbstractRockwell International has long endeavored to stimulate industrial utilization of space for materials processing. A successful introductory briefing program to acquaint nonaerospace industry with the space environment, microgravity process phenomena, experiment hardware, and the programs available to conduct research in space has encouraged several companies to initiate space processing research projects.To help satisfy industry's microgravity experiment hardware requirements, Rockwell has developed a multipurpose materials processing laboratory for use on the Space Shuttle. The Fluids Experiment Apparatus (FEA) has been flown to perform floating zone crystal growth and purification research and is currently being used to support further crystal growth research with advanced materials for Rockwell. Other companies are preparing experiments that are expected to be conducted in the FEA on future Space Shuttle missions.Rockwell is developing, with NASA, a program that will allow industry to plan and fly microgravity materials processing experiments within a few months–much faster than the current one to two year lead time. This low-cost program, patterned after the NASA Joint Endeavor Program, provides Space Shuttle flight services and use ot the FEA to conduct scientific investigations. Rockwell plans to offer experiment integration and support services to industry as needed.


1984 ◽  
Vol 31 (6) ◽  
pp. 1178-1182 ◽  
Author(s):  
John W. Adolphsen ◽  
John J. Yagelowich ◽  
Kusum Sahu ◽  
W. A. Kolasinski ◽  
R. Koga ◽  
...  

1992 ◽  
Author(s):  
J. L. Boynton ◽  
R. Tabibzadeh ◽  
S. T. Hudson

The cold air test program was completed on the SSME (Space Shuttle Main Engine) HPFTP (High Pressure Fuel Turbopump) turbine with production nozzle vane rings and polished coated rotor blades with a smooth surface finish of 30 microinch (0.76 micrometer) RMS (Root Mean Square). The smooth blades were polished by an abrasive flow machining process. The test results were compared with the air test results from production rough coated rotor blades with a surface finish of up to 400 microinch (10.16 micrometer) RMS. Turbine efficiency was higher for the smooth blades over the entire range tested. Efficiency increased 2.1 percentage points at the SSME 104 percent RPL (Rated Power Level) condition. This efficiency improvement could reduce the SSME HPFTP turbine inlet temperature by 57 degrees Rankine (32 degrees Kelvin) increasing turbine durability. The turbine flow parameter increased and the mid-span outlet swirl angle became more axial with the smooth rotor blades.


1992 ◽  
Author(s):  
H. MCCONNAUGHEY ◽  
J. LEOPARD ◽  
R. LIGHTFOOT

1993 ◽  
Vol 115 (3) ◽  
pp. 614-620 ◽  
Author(s):  
J. L. Boynton ◽  
R. Tabibzadeh ◽  
S. T. Hudson

The cold air test program was completed on the SSME (Space Shuttle Main Engine) HPFTP (High-Pressure Fuel Turbopump) turbine with production nozzle vane rings and polished coated rotor blades with a smooth surface finish of 30 μin. (0.76 μm) rms (root mean square). The smooth blades were polished by an abrasive flow machining process. The test results were compared with the air test results from production rough-coated rotor blades with a surface finish of up to 400 μin. (10.16 μm) rms. Turbine efficiency was higher for the smooth blades over the entire range tested. Efficiency increased 2.1 percentage points at the SSME 104 percent RPL (Rated Power Level) conditions. This efficiency improvement could reduce the SSME HPFTP turbine inlet temperature by 57 R (32 K), increasing turbine durability. The turbine flow parameter increased and the midspan outlet swirl angle became more axial with the smooth rotor blades.


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