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EVALUATION OF INJECTOR PRINCIPLES IN A 2400-POUND-THRUST ROCKET ENGINE USINJG LIQUID OXYGEN AND LIQUID AMMONIA (Record no. 398726)

000 -LEADER
fixed length control field 00568pam a2200145a 44500
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number NASA
Item number MEMO 12-11-58E
100 ## - MAIN ENTRY--PERSONAL NAME
Personal name Hendricks,Robert C,Ehlers,Robert C
245 1# - TITLE STATEMENT
Title EVALUATION OF INJECTOR PRINCIPLES IN A 2400-POUND-THRUST ROCKET ENGINE USINJG LIQUID OXYGEN AND LIQUID AMMONIA
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc.
Name of publisher, distributor, etc. Nasa, Washington, D.C.
Date of publication, distribution, etc. 1959
300 ## - PHYSICAL DESCRIPTION
Extent 33
500 ## - GENERAL NOTE
General note Bound With Nasa Memo 12-8-58e-12-10-58e, 12-13-58e-12-29-58e Lack No.12-9-58e, 12-12-58e, 12-14-58e-12-20-58e, 12-25-58e-12-28-58e.
700 ## - ADDED ENTRY--PERSONAL NAME
Personal name Graham,Robert W
964 ## -
-- CIRC
997 ## -
-- TR14064 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Withdrawn status Lost status Damaged status Not for loan Collection code Permanent Location Current Location Date acquired Full call number Barcode Date last seen Price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
    Untraceable   General Stacks PK Kelkar Library, IIT Kanpur PK Kelkar Library, IIT Kanpur 2007-08-12 NASA MEMO 12-11-58E TR14064 2016-05-19 2016-05-19 Technical Report

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