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 _______________________________________________ ERPS-list mailing list [EMAIL PROTECTED] http://lists.erps.org/mailman/listinfo/erps-list