The Dodge Viper first began production in 1992, with more than 14,000 sold to date. The 2003 SRT-10 is a two-seat convertible with 505-cubic inch all-aluminum V-10 engine producing no less than 500 horsepower and 500 pound-feet of torque. The 2003 Dodge Viper goes on sale in the Fall of 2002. The Dodge Viper Competition Coupe is a single-seat racing version of the SRT-10 convertible, but wrapped in fully enclosed coupe bodywork and designed exclusively for GT-class racing. Viper Competition Coupe performance estimates: 0-60 mph in 3.8 sec.; 0-100 mph in 9.2 sec.; 60-0 in 90 ft.; 100-0 mph in 260 ft. and top speed of 193 mph.
Base Price : $100,000
Engine : V10, OHV, front engine RWD
Displacement : 8,275 cc
Valve : 20 valves, 2 valves per cylinder
Transmission : 6-spd manual
Horsepower : 520 hp @ 5600 rpm(competition coupe), 500 hp(SRT-10)
Torque : 540 lb-ft @ 4600 rpm(competition coupe), 500 lb-ft(SRT-10)
Redline : 6100 rpm(competition coupe), 6000 rpm(SRT-10)
Top speed : 192 mph(competition coupe)
0-60 mph : 3.8 sec.(competition coupe)
0-¼ mile : 11.8 sec @ unknown(competition coupe), 11.9 sec.(SRT-10)
60-0 braking distance : 90 ft.(competition coupe)
Curb Weight : 3200 lbs(competition coupe), 3357 lbs(SRT-10)
Overall length : 184.1 in.
Wheelbase : 98.8 in.
Overall Width : 77.2 in.
Height : 46.7 in.
The Lockheed Martin F-16 Fighting Falcon -- nicknamed the "Viper" -- is a compact, multiple-role fighter aircraft. It is highly maneuverable and has proven itself in air-to-air combat and air-to-surface attack. The F-16 first flew in 1976, and to date, more than 4,000 have been built. It has a cost of approximately $25 million. Made in both single-seat and two-seat configurations, the F-16 is considered by many to be the most agile modern fighter, capable of withstanding up to 9 Gs, which exceeds the capability of all other current fighter aircraft. It has compiled a 71-0 air combat record.
Base Price: $14.6 million(F-16A/B), $18.8 million(F-16C/D)
Primary Function : Multirole fighter
Builder : Lockheed Martin Corp.
Power Plant : Pratt and Whitney F100-PW-200/220/229 or General Electric F110-GE-100/129(F-16C/D)
Thrust : 27,000 lbs(F-16C/D)
Speed : 1500 mph (Mach 2 at altitude)
Ceiling : Above 50,000 ft
Maximum Takeoff Weight : 37500 lbs
Range : More than 2,000 miles ferry range (1,740 nautical miles)
Armament : One M-61A1 20mm multibarrel cannon with 500 rounds; external stations can carry up to six air-to-air missiles, conventional air-to-air and air-to-surface munitions and electronic countermeasure pods
Length : 49 feet 5 inches
Height : 16 feet
Wingspan : 32 feet 8 inches
Crew : F-16C, one; F-16D, one or two
Date Deployed : January 1979