Thread
:
Gas turbines for assisting rockets.
View Single Post
#
14
October 11th 04, 05:03 PM
Len Lekx
external usenet poster
Posts: n/a
On Mon, 11 Oct 2004 12:40:43 GMT,
h (Rand
Simberg) wrote:
Which got me to thinking - could it be turned around...? Add a
supplementary oxidizer to current turbojet engine designs? This way,
Congratulations. You just reinvented the MIPPC concept, which is
being shown to not be very useful on the DARPA RASCAL program.
Ahhh... I didn't know it had already been tried. :-)
Len Lekx