000 00418pam a2200145a 44500
082 _aNASA
_bTN D-626
100 _aAdams,James J
245 1 _aSATELITE ATITUDE CONTROL USING A COMBINATION OF INERTIA WHEELS AND A BAR MAGNET
260 _a
_bNasa, Washington, D.C.
_c1960
300 _a42
500 _aBound With Nasa Tn D-621-625 & 627-630
700 _aBrissenden,Roy F
964 _gCIRC
997 _aTR12352 C
999 _c397695
_d397695