NASA NTRS · 19670000248
Rectilinear display gives acceleration load factor and velocity information
Abstract
Spacecraft entry monitoring system /EMS/ gives a rectilinear display of acceleration load factor and velocity information. This allows an astronaut to respond with manual spacecraft attitude corrective maneuver commands.
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Frank, A. J., Johnson, B. C.. 1967-07-01. Rectilinear display gives acceleration load factor and velocity information. https://ntrs.nasa.gov/citations/19670000248
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