A Digital Control Unit for a Rocket Borne Quadrupole Mass Spectrometer.
Abstract
To control a quadrupole mass spectrometer during a rocket flight a programmable digital control unit has been developed. The design centers around a programmable read only memory. Up to eight different programs of 16 breakpoints may be sequentially selected. For data transmission, a PCM system has been included into the control unit. The operation and the circuits of the unit are described. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1978
- Accession Number
- ADA057251
Entities
People
- J. Spencer Rochefort
- Raimundas Sukys
Organizations
- Northeastern University