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NASA Technical Note [NASA TN D-5641]: Analytical heat transfer investigation of insulated liquid methane wing tanks for supersonic cruise aircraft

By: Washington. National Aeronautics and Space Administration (NASA).

Contributor(s): Pleban, Eugene J.

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BookSeries: National Aeronautics and Space Administration ; NASA Technical Note. Publisher: Washington NASA 1970Description: 36p.Subject(s): Aircraft | Cryogenic fuels -- Liquid Methane | Supersonic transport

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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-5640 to 5649	Not for loan		TR8842

Total holds: 0

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Previous	An efficient method for computation of character tables of finite groups [NASA TN D-4763]	Microwave pump reqirements for field operational broadband rutile traveling wave masers [NASA TN D-4764]	EXPLORATORY STUDY OF PARALLEL-STAGE SEPARATION OF RESSABLE LAUNCH VEHICLES [NASA TN D-4765]	NASA Technical Note [NASA TN D-5641]: Analytical heat transfer investigation of insulated liquid methane wing tanks for supersonic cruise aircraft	NASA Technical Note [NASA TN D-5642]: An adaptive random-search algorithm for implementation of the maximum principle	NASA Technical Note [NASA TN D-5643]: Design and performance analysis of a medium-power dc-dc converter	NASA Technical Note [NASA TN D-5644]: Tests of a single-tube-in-shell water boiler with helical-wire insert, inlet nozzle and two different inlet-region plugs	Next

Bound together NASA TN D-5640 to 5649

Bound vol. Acc. No. 101183 contains Acc. No. TR8842 to TR8850

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