jangofett287
Heat shield 'tester'
- Joined
- Oct 14, 2010
- Messages
- 1,150
- Reaction score
- 13
- Points
- 53
My worry was that air might catch in the gap between the fuselage and the intake, but you look like you've got it all planned out. :thumbup:
wow that looks unstable, wing chord so far behind the vessel? must have some pretty heavy kit at the back to balance the whole thing out
Yeah, yaw and pitch stability would obviously require heavy augmentation; on the other hand, the role should be relatively stable with the CM location and the moderate anhedral.
Can someone explain to me why so many people like to measure things in nanometres?which leads me to the front edge of that SCRAM intake thing, it can stil work, but the bit above it should be dragged forward to split the air before it hits a flat piece of hull, else you would find your SCRAM engine about 1000nm from your landing site
Duhhhh.... :facepalm:it wasnt nanometers, its nautical miles
So it should be "NM" or "nmi", and not "nm", to avoid the confusion.it wasnt nanometers, its nautical miles
the old visor was good, but a little tweaking would be nice:
it should really fit exactly to the windshield and its surrounding panel, any exposed edge or face will be torn apart at mach 7 or so (leaving your self-respect in ruin) or at least ruin your aero-shockwave which could have devastating effects on re-entry heat loading and/or aerodynamics
which leads me to the front edge of that SCRAM intake thing, it can stil work, but the bit above it should be dragged forward to split the air before it hits a flat piece of hull, else you would find your SCRAM engine about 1000nm from your landing site
nice work though overall, that is sensational