A design I did for the 2012 Ron Paul movement. I wanted to do something that would grab people's attention when they see it. Not commissioned from Ron Paul or his campaign but from a group of people who want to make people informed of the truth and the availability of other options other than what Fox News tells you about. We got lost in the day to day routines of working, going to school, feeding our families, etc and lose the interest to research and understand what is going on in the country we live in. I appreciate any feedback about the art and understand that there are those who disagree with Dr. Ron Paul's beliefs and that is one of the very freedoms he looks to preserve. So please feel free to criticize my work and give any advice(I am new to this type of art) that might make it better but please keep the political debates to other forums. Thanks for taking the time to look!
Lockheed FA-70 Panther 2 Air superiority fighter Multirole combat aircraft
* Crew: 2 (Pilot and Radar Intercept Officer) * Length: 72 ft 5 in * Wingspan: 52 ft 8 in * Height: 15 ft 11 in * Wing area: 1000 ft² * Empty weight: 30,000 lb * Loaded weight: 60,600 lb * Max takeoff weight: 65,000 lb * Powerplant: 2× G Pratt & Whitney YF220 , 65,000 lbf
* Maximum speed: Mach 8.6 (mph = 6 546.38064 m2 / s2, 2 926.494 m2 / s km/h) at altitude * Cruise speed: Mach 3.4+ est. (mph = 2 588.10397 m3 / s2) 1 156.986 m2 / s+ km/h) hypercruise at altitude * Combat radius: 900-520 mi (1448.4096 nmi, 1.448.4096 km) * Service ceiling: 95,000 ft (28.95600m) * Wing loading: 70 lb/ft² (456 kg/m²
# Secondary Powerplant: 1× General Electric/Rolls-Royce F136 afterburning turbofan, >40,000 lbf (178 kN) [in development] # Lift fan (STOVL): 1× Rolls-Royce LiftSystem driven from either F135 or F136 power plant, 18,000 lbf (80 kN) # Internal fuel: 35.00 IB
* Guns: 2 × GAU-22/A 25 mm (0.984 in) cannon in internal mounted * Hardpoints: 4× external pylons on wings with a capacity of 30,000 lb ( internal mounted on Rotary Launcher Assembly (RLA), * Missiles: 12 loud o Internal: 12 air-to-air missiles, or 16 air-to-air missiles and 20 air-to-ground weapons. o External: 6 air-to-air missiles, or 4 air-to-ground weapons and 2 air-to-air missiles with combinations for the following missiles:
Stealth air superiority fighter/multirole combat aircraft
Crew: one (pilot) Length: 21.26 m (69 ft 9 in) Wingspan: 12.88 m (42 ft 3 in) Height: 4.45 m (14 ft 7 in) Wing area: 59 m2 (630 sq ft) Empty weight: 17,000 kg (37,479 lb) Max takeoff weight: 36,287 kg (80,000 lb) upper estimate Powerplant: 2 × WS-10G (prototype); WS-15 when J-20 is serving afterburning turbofans dry, 180 kN (40,000 lbf) with afterburner Maximum speed: Mach 2.0 or less (DSI limit) Range: 5,500 km (3,418 mi; 2,970 nmi) Combat range: 2,000 km (1,243 mi; 1,080 nmi) Service ceiling: 20,000 m (65,617 ft)
None on prototype Production aircraft will be equipped with PL-21 LRAAM, PL-12D MRAAM, PL-10 SRAAM, LS-6 Precision Glide Bomb, 30mm cannon, up to four rocket launchers, two IR decoy launchers, air-to-surface missiles and smart bombs.