High temperature rhenium material properties

34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 1998, Pages

  Biaglow, James A ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CHEMICAL VAPOR DEPOSITION; CREEP TESTING; FATIGUE OF MATERIALS; POWDER METALLURGY; PROPULSION; ROCKETS; SINTERING;

CREEP RUPTURES; ELEVATED TEMPERATURE; HIGH TEMPERATURE; HOT ISOSTATIC PRESSURE; LOW CYCLE FATIGUES; MATERIAL PROPERTY DATUM; RHENIUMS (RE); SUBSTRATE MATERIAL;

RHENIUM;

EID: 84963819574     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. Biaglow, J. A. Rhenium Material Properties, NASA TM-107043, AIAA paper 95-2398, July 1995
2. Reed, B. D. and Biaglow, J. A., Rhenium Mechanical Properties And Joining Technology, NASA TM- 107317, AIAA paper 96-2598, July 1996
3. Chazen, M.L, Material Property Test Results of Rhenium, AIAA paper 95-3356, July 1995
4. Chazen, M.L. and Sicher, D. High Performance Bipropellant Engine. AIAA paper 98-3356, July 1998
5. ASTM Standards, Standard Test Methods For Tension Testing of Metallic Materials, ASTM designation E8-98
6. Mittendorf, D. The Effect of Manufacturing Processing on the Mechanical Integrity of Rhenium, AIAA paper 97-2675, July 1997