At 09:08 PM 1/25/2004 -0800, you wrote:
    This engine, developed by Rocketdyne for BMD, is the subject of a brief
article in AW&ST, 12 January 2004, page 44.

    Thrust:     1,100 lbf
    Length:     8 inches
    Chamber P: ~500psi
    Fuel:       N2O4 & MMH
    Nozzle:     Metal, coated, rad-cooled

Chris W

Yes, very impressive.


The engines on our vehicle now only have a T/W of 35, even when operated at fairly high pressure. We do count the valve in the engine weight, which is fairly significant. We could double this T/W without heroic effort, but going much beyond that would be hard with a catalyst based motor.

John Carmack

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