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Previous Record |
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| Title: |
A DESIGN AND PERFORMANCE STUDY OF THE NUCLEAR DIRECT-AIR-CYCLE SUPERSONIC AIRPLANE, INCLUDING THE EFFECTS OF OPERATING TEMPERATURES AND FUEL PLATE MATERIAL AND THICKNESS
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| Author(s): |
Manson, S. V.; Wachtl, W. W.
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| Abstract: |
Nuclear direct-air-cycle supersonic aircraft design study - effect of temperature and fuel plate material
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| NASA Center: |
Glenn Research Center
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| Publication Date: |
Mar 1, 1953
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| Document Source: |
CASI |
| No Digital Version Available: |
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| Document ID: |
19630008768
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| Accession ID: |
63N18645
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| Publication Information: |
Number of Pages = 73 |
| Report Number: |
NACA-RM-E53C18
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| Price Code: |
A04 |
| Keywords: |
AIRCRAFT DESIGN; INTERMETALLICS; NUCLEAR PROPELLED AIRCRAFT; OPERATING TEMPERATURE; SUPERSONIC AIRCRAFT; TEMPERATURE EFFECTS; THICKNESS; NUCLEAR AIRCRAFT; SUPERSONIC AIRCRAFT;
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| Notes: |
NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS. LEWIS FLIGHT PROPULSION LAB., CLEVELAND, OHIO A DESIGN AND PERFORMANCE STUDY OF THE NUCLEAR DIRECT-AIR-CYCLE SUPERSONIC AIRPLANE, INCLUDING THE EFFECTS OF OPERATING TEMPERATURES AND FUEL PLATE MATERIAL AND THICKNESS S. V. MANSON AND WILLIAM W. WACHTL WASHINGTON, NACA, MAR. 1953 73P 17 REFS /NACA RM E53C18/ /DECLASSIFIED/ OTS- 7.60 PH, 2.39 MF |
| Accessibility: |
Unclassified; No Copyright; Unlimited; Publicly available; |
| Updated/Added to NTRS: |
2006-11-06 |
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