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|a NAS 1.15:89894
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| 100 |
1 |
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|a Graham, Ronald E.
|q (Ronald Edward)
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| 245 |
1 |
0 |
|a Effect of gimbal friction modeling technique on control stability and performance for Centaur upper-stage
|h [microform] /
|c Ronald E. Graham.
|
| 260 |
|
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|a [Washington, DC] :
|b National Aeronautics and Space Administration ;
|a [Springfield, Va. :
|b For sale by the National Technical Information Service,
|c 1987]
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| 300 |
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|a 1 v.
|
| 440 |
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0 |
|a NASA technical memorandum ;
|v 89894.
|
| 500 |
|
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|a Distributed to depository libraries in microfiche.
|
| 533 |
|
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|a Microfiche.
|b [Washington, D.C.? :
|c National Aeronautics and Space Administration],
|d 1987.
|e 1 microfiche.
|
| 650 |
|
0 |
|a Launch vehicles (Astronautics)
|
| 710 |
1 |
|
|a United States.
|b National Aeronautics and Space Administration.
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|a mcgd afig-r-
|c NAS 1.15:89894
|b mq6311785
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|y 6311785
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