Chicoartist:
Hi. Well, the engine used in 1951 was an earlier version of the J-33 engine than we had in our birds, so it may have been different, but on ours, the engine was started using a separate
fuel control unit, known as the Starting Fuel Control, with the throttle in the cutoff position. After the engine lit off and progressed to a certain RPM, the throttle lever was brought "around the horn" into idle, which activated the Main Fuel Control. The Starting Fuel switch was then deactivated. There was no tankage for a different grade of fuel on our birds, and no place to mount one that I can think of. Things are packed in pretty tight. The gyro for the heading indicator system even had to be mounted in the engine bay!
I do remember reading that the early engines were very sensitive to throttle movements, and if one advanced the throttle too fast it could cause a flameout. Our aircraft had a fuel control that compensated for that. One of our ground run checks was to ram the throttle full forward as fast as you could to check this out. Always a lot of fun! One time I was doing a run in the middle of winter (which at the Griff meant 10-20 below zero!). When I did the full throttle check, the left wing suddenly dropped, almost putting the tip tank on the ground. I did a quick emergency shutdown, thinking that the turbine wheel had disintegrated and sheared off the rear fuselage or something, but it turned out that the vibration had caused the cold and brittle left main landing gear strut seals to suddenly allow the nitrogen precharge in the strut to leak out. (This is basically what happened to the Space Shuttle Challenger in 1986 when the cold seals in the solid rocket booster allowed it to leak exhaust gas.)
Hope you find this of use!
Russ