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NASA Technical Note [D- 251-260] (Record no. 565851)

000 -LEADER
fixed length control field 02057nam a22002897a 4500
003 - CONTROL NUMBER IDENTIFIER
control field OSt
040 ## - CATALOGING SOURCE
Transcribing agency IIT Kanpur
041 ## - LANGUAGE CODE
Language code of text/sound track or separate title eng
110 ## - MAIN ENTRY--CORPORATE NAME
Corporate name or jurisdiction name as entry element Washington. National Aeronautics and Space Administration (NASA)
245 ## - TITLE STATEMENT
Title NASA Technical Note [D- 251-260]
260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT)
Place of publication Washington
Name of publisher NASA
Year of publication 1960
440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE
Title National Aeronautics and Space Administration
440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE
Title NASA Technical Note
500 ## - GENERAL NOTE
General note NASA TN D-251 -- A summary of operating conditions experienced by two helicopters in a commercial and a military operation/ Andrew B. Connor and LeRoy H. Ludi
500 ## - GENERAL NOTE
General note NASA TN D-252 -- Investigation of the natural frequencies of fluids in spherical and cylindrical tanks/ John Locke McCarty and David G. Stephens
500 ## - GENERAL NOTE
General note NASA TN D-253 -- Longitudinal range control during the atmospheric phase of a manned satellite reentry/ Arthur Assadourian and Donald C. Cheatham
500 ## - GENERAL NOTE
General note NASA TN D-254 -- An analysis of nose ablation for ballistic vehicles/ Leonard Roberts
500 ## - GENERAL NOTE
General note NASA TN D-255 -- Requirements of trajectory corrective impulses during the approach phase of an interplanetary mission/ Alan L. Friedlander and David P. Harry, III
500 ## - GENERAL NOTE
General note NASA TN D-256 -- Fatigue damage during complex stress histories/ H. W. Liu and H. T. Corten
500 ## - GENERAL NOTE
General note NASA TN D-257 -- Performance investigation of a nonpumping rocket-ejector system for altitude simulation/ Anthony Fortini
500 ## - GENERAL NOTE
General note NASA TN D-258 -- Propellant vaporization as a criterion for rocket-engine design: experimental effect of combustor length, throat diameter, injection velocity, and pressure on rocket combustor efficiency/ Bruce J. Clark
500 ## - GENERAL NOTE
General note NASA TN D-259 -- Rolling-contact fatigue life of a crystallized glass ceramic/ Thomas L. Carter and Erwin V. Zaretsky
500 ## - GENERAL NOTE
General note NASA TN D-260 -- Continued study of advanced-temperature nickel-base alloys to investigate vanadium additives/ John C. Freche, Thomas J. Riley and William J. Waters
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical Term Aeronautics
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical Term Spacecraft
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type Books
Holdings
Withdrawn status Lost status Damaged status Not for loan Collection code Permanent Location Current Location Date acquired Serial Enumeration / chronology Accession Number Koha item type
        COMPACT STORAGE (BASEMENT) PK Kelkar Library, IIT Kanpur PK Kelkar Library, IIT Kanpur 2022-07-08 NASA TN D- 251-260 63649 Technical Report

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