| 000 -LEADER |
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| fixed length control field |
00615nam a22001697a 4500 |
| 005 - DATE AND TIME OF LATEST TRANSACTION |
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| control field |
20200212145716.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
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| fixed length control field |
200212b xxu||||| |||| 00| 0 eng d |
| 040 ## - CATALOGING SOURCE |
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| Transcribing agency |
IIT Kanpur |
| 041 ## - LANGUAGE CODE |
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| Language code of text/sound track or separate title |
eng |
| 100 ## - MAIN ENTRY--AUTHOR NAME |
|---|
| Personal name |
Buglia, Jmes J. and Newcomb, John F. |
| 245 ## - TITLE STATEMENT |
|---|
| Title |
A method for determinig the propellant required to maintain an earth orbital vehicle in a useful orbirt between two specified altitude limits [NASA TN D-1817] |
| Statement of responsibility, etc |
James J. Buglia and John F. Newcomb |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) |
|---|
| Place of publication |
Washington, D. C. |
| Name of publisher |
NASA |
| Year of publication |
August 1963 |
| 300 ## - PHYSICAL DESCRIPTION |
|---|
| Number of Pages |
31p |
| 505 ## - FORMATTED CONTENTS NOTE |
|---|
| Formatted contents note |
Technica note D-1817 |
| 700 ## - ADDED ENTRY--PERSONAL NAME |
|---|
| Personal name |
Newcomb, John F. |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) |
|---|
| Koha item type |
Reference |
