000 -LEADER |
fixed length control field |
00625pam a2200181a 44500 |
003 - CONTROL NUMBER IDENTIFIER |
control field |
OSt |
005 - DATE AND TIME OF LATEST TRANSACTION |
control field |
20220822142958.0 |
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
fixed length control field |
220822b xxu||||| |||| 00| 0 eng d |
040 ## - CATALOGING SOURCE |
Transcribing agency |
IIT Kanpur |
041 ## - LANGUAGE CODE |
Language code of text/sound track or separate title |
eng |
100 ## - MAIN ENTRY--AUTHOR NAME |
Personal name |
Yancey, Roxaanah B, |
245 1# - TITLE STATEMENT |
Title |
AERODYNAMIC-DERIVATIVE CHARACTERISTICS OF THE X-15 RESEARCH AIRPLANE AS DETERMINED FROM FLIGHT TESTS FOR MACH NUMBERS FROM 0.6 TO 3.4 [NASA TN D-1010] |
Statement of responsibility, etc |
Roxanah B. Yancey |
260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) |
Name of publisher |
National Aeronautics and Space Administration |
Year of publication |
1962 |
Place of publication |
Washington, D.C. |
300 ## - PHYSICAL DESCRIPTION |
Number of Pages |
68p |
500 ## - GENERAL NOTE |
General note |
Bound With NASA TN D-1051-1060 |
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
Topical Term |
Aerodynamic |
942 ## - ADDED ENTRY ELEMENTS (KOHA) |
Koha item type |
Technical Report |