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P8E-9
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 .
