VEVAK
SENIOR MEMBER
- Joined
- Oct 24, 2013
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1960’s US technology:
D-21 and D-21B without booster
- Wingspan: 19 ft 0.25 in (5.8 m)
- Length: 42 ft 10 in (13.1 m)
- Height: 7 ft 0.25 in (2.1 m)
- Launch weight: 11,000 lb (5,000 kg)
- Maximum speed: Mach 3.35 (2,300 mph; 3,600 km/h; 2,000 kn) (conversions estimated at the service ceiling altitude)
- Service ceiling: 95,000 ft (29,000 m)
- Range: 3,000 nmi (3,500 mi; 5,600 km)
- Engine: 1 x Marquardt RJ43-MA-20S4 ramjet, 1,500 lbf (6.7 kN)
Wether it’s flying wing or delta wing, my idea would be a force multiplier creating synergies with the BM force. If Iran implements my idea (swarm based high altitude supersonic UCAVs) it would be one of the greatest assets for the Republic.
On the other hand, brand new tanks would be a waste that would sit and decay in military bases only to be rolled out in few numbers for war games and would create no additional deterrence effect.
Your comparing that design to a potential flying wing design capable of Mach 2 and you assume it makes no difference? LOL!
The fact that you haven't yet matured enough nor educated yourself enough to see the absurdity of even attempting to build a flying wing design capable of Mach 2(hi altitude) especially at Iran's level of technology speaks for itself. And the fact that your showing a high angled relatively short winged low drag Aircraft as some kind of proof of validity to your concept shows your immaturity on the subject. pass nazar nadee sangeen tar e!
And just incase you didn't comprehend, in no way am I saying it's technology not possible! Simply that it's not feasible!