000 -LEADER |
fixed length control field |
00593pam a2200205a 44500 |
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
fixed length control field |
160408b1986 xxu||||| |||| 00| 0 eng d |
020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
International Standard Book Number |
0444426191 |
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER |
Classification number |
629.411 |
Item number |
J963o |
100 ## - MAIN ENTRY--PERSONAL NAME |
Personal name |
Junkins, John L. |
245 1# - TITLE STATEMENT |
Title |
OPTIMAL SPACECRAFT RATIONAL MANEUVERS |
260 ## - PUBLICATION, DISTRIBUTION, ETC. |
Place of publication, distribution, etc. |
Amsterdam |
Name of publisher, distributor, etc. |
Elsevier |
Date of publication, distribution, etc. |
1986 |
300 ## - PHYSICAL DESCRIPTION |
Extent |
xvii,515 |
440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE |
Title |
Studies In Astronautics |
Volume/sequential designation |
V. 3 |
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
Topical term or geographic name entry element |
Astrodynamics |
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
Topical term or geographic name entry element |
Space Vehicles -- Attitude Control Systems |
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
Topical term or geographic name entry element |
Rational Motion (Rigid Dynamics) |
700 ## - ADDED ENTRY--PERSONAL NAME |
Personal name |
Turner, James D. |
964 ## - |
-- |
CIRC |
997 ## - |
-- |
A111597 v. 3 C |