000 -LEADER |
fixed length control field |
00719nam a22002057a 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 |
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER |
Classification number |
NASA |
Item number |
TN D-1969 |
100 ## - MAIN ENTRY--AUTHOR NAME |
Personal name |
Adams, James J. |
245 ## - TITLE STATEMENT |
Title |
Simulator study of a satellite attitude control system using inertia wheels and a magnet [NASA TN D-1969] |
Statement of responsibility, etc |
James J. Adams, W. E. Howell and Hugh P. Bergeron |
260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) |
Place of publication |
Washington, D.C. |
Name of publisher |
National Aeronautics and Space Administration [NASA] |
Year of publication |
1963 |
300 ## - PHYSICAL DESCRIPTION |
Number of Pages |
16p |
440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE |
Title |
National Aeronautics and Space Administration [NASA] |
500 ## - GENERAL NOTE |
General note |
Bound with NASA TN D-1961-1970. Lack No.-1966 |
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
Topical Term |
Inertia wheels |
700 ## - ADDED ENTRY--PERSONAL NAME |
Personal name |
Howell, W. E. |
700 ## - ADDED ENTRY--PERSONAL NAME |
Personal name |
Bergeron, Hugh P. |
942 ## - ADDED ENTRY ELEMENTS (KOHA) |
Koha item type |
Technical Report |