| TRANSICOIL LLC | |
| MODERATELY RUGGED | |
| 1.250 POUNDS | |
| USAF | |
| TRANSMITTER ELECTRICAL DATA;ROTOR INPUT VOLTAGE 26 V;FREQ 400 HZ;INPUT IMPEDANCE 100 OHMS;TRANSFORMATION RATIO 0.454;PHASE SHIFT PLUS 5 DEG;NULL VOLTAGE 20 MV MAX;ELECTRICAL ERROR 2.8 MIN MAX;OUTPUT VOLTAGE REGULATION 10 PCT MAX;ALIGNMENT 4 ARC MIN MAX;RESOLVER ELECTRICAL DATA;INPUT VOLTAGE 10 V;FREQ 6250 HZ;INPUT IMPEDANCE 5000 OHMS;NULL VOLTAGE FUNDAMENTAL 0.4 MV;TOTAL NULL VOLTAGE 7.5 MV;TRANSFORMATION RATIO 0.5 MV;COMPENSATOR TRANSFORMATION RATIO 1.0 MV;ELECTRICAL ERROR 2 MIN MAX;DISTORTION 0.1 PCT MAX;D C RESISTANCE 30 OHMS MIN;PHASE SHIFT PORM 5 DEG MAX;BALANCE PORM 0.3 MAX;BODY DIM.;SHOULDER DIA 1.312 IN. MAX;PILOT DIA 0.875 IN. MAX;O/A LG 4.640 IN. MAX;FLANGE DIA 1.437 IN. MAX;FLANGE THK 0.093 IN.;UNDERCUT W 0.078 IN.;PILOT LG 0.04 IN.;SHOLDER LG 0.132 IN.;MTG SURFACE TO TERMINAL END 4.135 IN. MAX;ROUND 0.463 IN. LG SHAFT;17 WIRE LEAD TERMINALS;SHAFT RUNOUT 0.001 IN. MAX;SHAFT RADIAL PLAY 0.0008 IN. MAX;SHAFT END PLAY 0.001 IN. MAX |
