F117 - Some stats
Specifications
An orthographically projected diagram of the F-117A Nighthawk
General characteristics
* Crew: 1
* Length: 69 ft 9 in (20.08 m)
* Wingspan: 43 ft 4 in (13.20 m)
* Height: 12 ft 9.5 in (3.78 m)
* Wing area: 780 ft² (73 m²)
* Empty weight: 29,500 lb (13,380 kg)
* Loaded weight: 52,500 lb (23,800 kg)
* Powerplant: 2× General Electric F404-F1D2 turbofans, 10,600 lbf (48.0 kN) each
Performance
* Maximum speed: Mach 0.92 (617 mph, 993 km/h)
* Cruise speed: Mach 0.92
* Range: 930 NM[37] (1720 km)
* Service ceiling 69,000 ft (20,000 m)
* Wing loading: 65 lb/ft² (330 kg/m²)
* Thrust/weight: 0.40
Armament
* 2× internal weapons bays with one hardpoint each (total of two weapons) equipped to carry:
o Bombs:
+ BLU-109 hardened penetrator
+ GBU-10 Paveway II laser-guided bomb
+ GBU-12 Paveway II laser-guided bomb
+ GBU-27 Paveway III laser-guided bomb
+ JDAM INS/GPS guided munition
F35 - some stats
General characteristics
* Crew: 1
* Length: 50 ft 6 in (15.37 m)
* Wingspan: 35 ft 0 in (10.65 m)
* Height: 17 ft 4 in (5.28 m)
* Wing area: 459.6 ft² (42.7 m²)
* Empty weight: 29,000 lb A; 32,200 lb B; 32,100 lb C[75] (13,200 kg A; 14,600 kg B; 14,600 kg C)
* Loaded weight: 44,400 lb (20,100 kg)
* Max takeoff weight: 60,000 lb (27,200 kg)
* Powerplant: 1× Pratt & Whitney F135 afterburning turbofan
o Dry thrust: 25,000 lbf[22] (111 kN)
o Thrust with afterburner: 40,000+ lbf[22] (178+ kN)
* Secondary Powerplant: 1× General Electric/Rolls-Royce F136 afterburning turbofan, >40,000 lbf (178 kN) [in development]
* Lift fan (STOVL): 1× Rolls-Royce Lift System driven from either F135 or F136 power plant, 18,000 lbf (80 kN)
Performance
* Maximum speed: Mach 1.6+[22] (1,200 mph, 1,931 km/h)
* Range: A: 1,200 nmi; B: 900 nm; C: 1400 nm[22] (A: 2,200 km; B: 1,667 km; C: 2,593 km) on internal fuel
* Combat radius: 600 nmi (690 mi, 1,110 km)
* Rate of climb: classified (not publicly available)
* Wing loading: 91.4 lb/ft² (446 kg/m²)
* Thrust/weight:
o With full fuel: A: 0.89; B: 0.92; C: 0.81[22]
o With 50% fuel: A: 1.12; B: 1.10; C: 1.01[22]
g-Limits[76]
* F-35A: 9 g
* F-35B: 9 g
* F-35C: 9 g
Armament
* Guns: 1 × GAU-12/U 25 mm cannon slated to be mounted internally with 180 rounds in the F-35A and fitted as an external pod with 220 rounds in the F-35B and F-35C.[22]
* Hardpoints: 6 with a capacity of 15,000 lb (6,800 kg)[22],
* Missiles: Internal: 6 air-air missiles or 2 air-air missile and 2 air-surface weapons; External: 2 missiles and 4 missiles/bombs[22]
I think it's clear which is the more capable aircraft. My point, as before, is not the ability of the aircraft, but the ability to purchase it in large enough numbers to make a real difference.