SpaceShipOne "...is powered by a hybrid rocket motor. The innovative engine uses a solid, rubbery hydroxy-terminated polybutadiene propellant and nitrous oxide laughing gas as the oxidizer." One news report I read said the rubbery propellant is solid and is in a hollow tube. Does anyone know how this is metered out into the combustion chamber? Stan rtejera@xxxxxxxxxxx wrote: >Looks like it was a smooth flight all around, Reached apogee of 368,000 = >ft.=20 > >http://spaceflightnow.com/ss1/status.html > >Rick Tejera >International Dispatcher/Customer Service Rep >UPS Logistics >800-528-6041 >480-315-5162 > >-- >See message header for info on list archives or unsubscribing, and please >send personal replies to the author, not the list. > > > > > -- See message header for info on list archives or unsubscribing, and please send personal replies to the author, not the list.