> > POGO will be constant pressure, not blow-down. Planned > deliverable T/W at liftoff will be 1.5; one of our big design challenges > will be getting the engines to throttle low enough to land. It's intended > to have a pretty good mass fraction -- probably higher than most HPR rockets.
Deep throttling is absolutely trivial with peroxide monoprop issues. Don't worry about it at all. John Carmack _______________________________________________ ERPS-list mailing list [EMAIL PROTECTED] http://lists.erps.org/mailman/listinfo/erps-list
