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PERFORMANCE OF A 48-MODULE SWIRL-CAN TURBOJET COMBUSTOR SEGMENT AT HIGH TEMPERATURES USING ASTM-A1 FUEL. (Record no. 397091)

000 -LEADER
fixed length control field 00461pam a2200145a 44500
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number NASA
Item number TN D-5597
100 ## - MAIN ENTRY--PERSONAL NAME
Personal name Niedzwiecki,Richard W
245 1# - TITLE STATEMENT
Title PERFORMANCE OF A 48-MODULE SWIRL-CAN TURBOJET COMBUSTOR SEGMENT AT HIGH TEMPERATURES USING ASTM-A1 FUEL.
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc.
Name of publisher, distributor, etc. Nasa, Washington, D.C.
Date of publication, distribution, etc. 1969
300 ## - PHYSICAL DESCRIPTION
Extent 38
500 ## - GENERAL NOTE
General note Bound With Nasa Tn D-5590-96, 5598-99 Lack No.5594
700 ## - ADDED ENTRY--PERSONAL NAME
Personal name Moyer,Harry M
964 ## -
-- CIRC
997 ## -
-- TR12671 C
Holdings
Withdrawn status Lost status Damaged status Not for loan Collection code Permanent Location Current Location Date acquired Full call number Barcode Date last seen Price effective from Koha item type
        General Stacks PK Kelkar Library, IIT Kanpur PK Kelkar Library, IIT Kanpur 2007-08-12 NASA TN D-5597 TR12671 2016-05-19 2016-05-19 Technical Report

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