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An inflight data recording system for tubeflight vehicles

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PROXIMITY TRANSDUCERS .. (TO MEASURE YAW ANGLE ~~ AND LATERAL POSITION) . \ FIG. 20
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EIGHT CHANNEL TEL1"'METRY SYSTEM WITH FAILSAFE SYSTEM (Transmitter and Receiver) (Engineering Model) APPENDIX A…
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This report describes the operational procedures of an eight-channel telemetry system developed for monitoring the in-flight…
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OPERATING INSTRUCTIONS A. TELEMETRY RECEIVER The receiver has been pre-tuned for optimum operation with the vehicle…
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A-3 Pbssible Cause. a) No R.F. carrier at receiver input. b) Receiver no't tuned to R.F. carrier. (Only sligh-t…
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output plugs are in place, then the internal resistor is automatically disconnected and the external load is substituted.…
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A-5 C. TELEMETRY TRANSMITTER Before operating the transmitter for external test or for transmission in the tube, be sure the…
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D. FAILSAFE TRANSMITTER AND RECEIVER TRANSMITTER: 1) Set up with external power supply output connected to the input power…
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FAILSAFE RECEIVER: Before vehicle run, 'check reception of the failsafe signal at the failsafe receiver (on the vehicle…
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DiScrim- i nl; fo,-' Fig. 7. Receiver Block Diagram
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1:2. 10 -I Y1 pvi:. 1.: 0 V Co ( l/()/br.) Fig.'ll. System Linearity Channe~ 2 (2300 Hz) A-1S
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J.?. :Inpvt 1.0 VC 6 ( vo/·b:;) .. Fig,' 12, Sys tern Linearity Channel 3 (3000 Hz) A-19
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