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Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility (VKF) 40-inch supersonic and the 50-inch hypersonic wind tunnels A & C (IH-97A/B/C) / J. Marroquin.
Connect to full text Available online
View online- Format:
- Book
- Government document
- Author/Creator:
- Marroquin, J., author.
- Series:
- NASA contractor report ; NASA CR-167693.
- NASA/CR ; 167693
- Language:
- English
- Subjects (All):
- Von Karman Institute for Fluid Dynamics.
- Genre:
- Online resources.
- Physical Description:
- 1 online resource (iv, 164 pages) : illustrations.
- Place of Publication:
- Houston, Texas : Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, March 1985.
- Notes:
- "March 1985."
- "DMS-DR-2520."
- Includes bibliographical references (page 37).
- Description based on online resource, PDF version; title from title page (NASA, viewed Aug. 24, 2018).
- Other Format:
- Microfiche version: Marroquin, J. Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility (VKF) 40-inch supersonic and the 50-inch hypersonic wind tunnels A & C (IH-97A/B/C).
- OCLC:
- 1049803362
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