000 00635 a2200241 4500
001 329338
020 _a
041 _aeng
080 _aLNASA TP - 1978 : 1982
245 _aEffects of cable geometry and aircraft attitude on the accuracy of a magnetic leader cable system for aircraft guidance during rollout and turnoff
250 _a
260 _aWashington, D.C.
260 _bNASA
260 _c1982
300 _a30 p.
300 _c
856 _u
490 _aNASA TP - 1978 : 1982
700 _a
650 _a
650 _aMagnetic leader cable, Aircraft guidance, Avionics, Aircraft control system
942 _cPP
942 _2UDC
999 _c190834
_d190834