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Planet-B: Technical notes and drawingsThe design of the transformer designated as T101 (061-0351) in the Filament/Bias module (061-0119) in the Planet-B NMS instrument was verified because of the differences from the GCMS and INMS instrument designs. A breadboard of a representation of the Hybrid 2301065, Bias Drive A driving a 2N3700 NPN transistor, with dual 75V secondaries, with loads, was used to test the circuit. The initial transformer design that was wound with bifilar secondaries was too unstable to test. The second 1408 transformer with a split bobbin and the feedback winding below the primary was also found to be unstable. (It was nearly impossible to keep the circuit from squeeging). The third transformer tested has the feedback on the outside of the resonant winding. The primary goal of the design was to have as tight a magnetic coupling as possible to the resonant winding, and as loose a coupling as possible to the primary. Further, the circuit AC ground is connected to the winding at the feedback end of the secondary winding. This transformer proved to be very stable - it is virtually impossible to make this design squeg. An emitter resistor (Rl29A) was added to this circuit, as referenced to the GCMS design, to protect Q102 from thermal runaway in the event of a turn on with a non- resonate circuit or load short. This was verified to protect Q102 for at least 30 seconds in the event of a short. Approximately 1% of the 4lmW input power is lost in this protection resistor under normal operation. The circuit was verified to operate normally when a radiated Q102 (2N3700), (low Beta) transistor was substituted for the normal 2N3700. It should be noted that the monitored drive voltage went to approximately 2.7V with this low gain transistor.
Document ID
19960044500
Acquisition Source
Goddard Space Flight Center
Document Type
Contractor Report (CR)
Authors
Carignan, George R.
(Michigan Univ. Ann Arbor, MI United States)
Date Acquired
September 6, 2013
Publication Date
July 25, 1996
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
NASA-CR-201797
NAS 1.26:201797
Report Number: NASA-CR-201797
Report Number: NAS 1.26:201797
Accession Number
96N32013
Funding Number(s)
CONTRACT_GRANT: NAG5-2918
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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