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NASA Technical Note: COMPARATIVE STUDY OF FUSELAGE TANKS FOR LIQUID-METHANE-FUELED SUPERSONIC AIRCRAFT

By: Chambellan, Rene E.

Contributor(s): Bevevino, William A.

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BookSeries: National Aeronautics and Space Administration ; NASA Technical Note. Publisher: Washington, D.C. NASA 1968Description: 16p.Subject(s): Flight-Weight Nonintegral Tanks | Gage Pressures

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Item type	Current location	Collection	Call number	Vol info	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		NASA TN D-4837	Not for loan		TR7572

Total holds: 0

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Previous	NASA Technical Report [NASA TR R-104]: Local heat transfer and recovery temperatures on a yawed cylinder at a mach number of 4.15 and high Reynolds numbers	NASA Technical Report [NASA TR R-105]: Sputtering of metals by mass-analyzed N2+ and N+	NASA Technical Note: LANDING LOADS AND ACCELERATIONSOF THE XB-70-1 AIRPLANE	NASA Technical Note: COMPARATIVE STUDY OF FUSELAGE TANKS FOR LIQUID-METHANE-FUELED SUPERSONIC AIRCRAFT	NASA Technical Note: EXCITATION SPECTRUM FOR A BOSE GAS WITH REPULSIVE AND ATTRACTIVE INTERACTIONS	NASA Technical Note: INCOMPRESSIBLY LUBRICATED RAYLEIGH STEP JOURNAL BEARING	NASA Technical Note: HIGH-POWER KINETICS OF A TWO-DIMENSIONAL CIRCULATING-LIQUID-METAL-FUEL REACTOR	Next

Technical Note D-4831-4840

Bound Vol. No.101114 contents TR7567-7575

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