| 000 -LEADER |
|---|
| fixed length control field |
00617pam a2200181a 44500 |
| 005 - DATE AND TIME OF LATEST TRANSACTION |
|---|
| control field |
20200624121132.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
|---|
| fixed length control field |
200624b 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 |
Spearman, M. Leroy |
| 245 1# - TITLE STATEMENT |
|---|
| Title |
Aerodynamic characteristics in pitch of a series of cruciform-wing missiles with canard controls at a mach number of 2.01 [NASA TN D-839] |
| Statement of responsibility, etc |
M. Leroy Spearman |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) |
|---|
| Name of publisher |
Nasa |
| Year of publication |
1961 |
| Place of publication |
Washington, D.C. |
| 300 ## - PHYSICAL DESCRIPTION |
|---|
| Number of Pages |
40p |
| 440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE |
|---|
| Title |
National Aeronautics and space Administratio (NASA) |
| 505 ## - FORMATTED CONTENTS NOTE |
|---|
| Formatted contents note |
NASA technical report |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical Term |
cruciform-wing |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) |
|---|
| Koha item type |
Books |
