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P8E-9 -

Credit: Boeing / Rocketdyne. 9,067 bytes. 153 x 222 pixels.

Manufacturer Name: P8E-9. Designer: Rocketdyne. Developed in: 1964. Application: Lance. Propellants: Nitric acid/UDMH Isp (sea level): 238 sec. Comments: Lance Booster and Sustainer System. Pressure-fed. Sustainer 4400 -14,400 lbf, 227 sec Isp. Thrust and specific impulse values are at sea level.
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Last update 12 March 2001.
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© Mark Wade, 2001 .