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"Boom and Zoom: The History of the NF-104A AST"
John Terry White

It's apparent the J Terry White is defending ? vs Chuck Yeager

"The roll rockets were designed for a maximum thrust of 40 pounds and the pitch and yaw rockets for a maximum thrust of 113 lbs, at an altitude of 200,000 feet."

Jarvis, Calvin R.; Lock, Wilton P. (1965). Operational Experience With the X-15 Reaction Control and Reaction Augmentation Systems. NASA. OCLC 703664750. TN D-2864.

the large SERVICER job [...] first performed average-G navigation, then guidance equations, then throttle and attitude output, and then the updating of displays — each part using the outputs of the ones preceding.

Apollo 11 and Other Screw-Ups