The design concept and capabilities of a rocket-borne digital pressure
gage capable of measuring atmospheric pressures from 1 atm to 0.5 mm Hg
are described. The gage described is of the type devised by
Vanderschmidt (1959) and Cambou et al. (1964). Particular attention is
given to choice of instrumentation, preflight calibration, and flight
results. It is shown that the performance of the digital pressure
designed compares well with that of conventional meteorological pressure
gages. A major advantage of this pressure transducer is that its output
is digital and hence easy to transmit and count. It also has a wide
dynamic range of pressure measurements. The range of the instrument can
be extended to 0.01 mm Hg by connecting two ionization chambers in
parallel.