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During the 1960's NASA looked at several possible improvements to the existing Block II Apollo's. One such study was by Bell and looked into a new design for RCS thrusters, which was theoretically scaleable from 5lb to 1000lb of thrust.
Experimental auxiliary rocket engine, part I. Final report
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660021108_1966021108.pdf
Experimental auxiliary rocket engine, part II. Final report
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660021109_1966021109.pdf
Experimental auxiliary rocket engine, part I. Final report
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660021108_1966021108.pdf
Experimental auxiliary rocket engine, part II. Final report
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660021109_1966021109.pdf
