To avoid traction asymmetry, even the option of installing both engines in the fuselage was considered, but eventually, it was decided to give the problems of traction asymmetry and “non-starting” the air intake to the automatic air intake control system. The “non-start” of the air intakes remained the most vulnerable place of all A-12/YF-12/SR-71 series aircraft. Over time, these problems have been resolved only partially by selecting control coefficients in the control system and replacing the analog system with a digital one. Bill Weaver performed many risky flights under the air intake control system debugging program. In the flight, Weaver deliberately interrupted the state of “launch”: in his words, the feeling at the same time resembled the feelings of a passenger courier train rushing not on the rails, and on the sleepers.
By the end of 1967, Lockheed handed over the last, 31st, ordered SR-71 to the Air Force; the production line was shut down. Perhaps, it was not necessary t
