Back in the early 60's when the US Army needed a attack helicopter there were three entries, the AH-64, AH-56, and S-66. I do not have any info on
the S-66. As you all know the AH-64 won out but I want to tell abou the AH-56. The AH-56(name Cheyenne) had a crew of two. It featured a swiveling
gunner's station link to rotating belly and nose turrets. It also had a laser range finder tied to a fire control computer. The AH-56 hwas armed
with a 30mm automatic cannon in the belly turret and a 40mm grenade launcher or a 7.62mm gatling gun in the chin turret. It could also be armed with
TOWs or 2.75 inch rockets. The AH-56 had a single four- bladed main rotor, a anti-torque tail rotor, and a three-bladed pusher. It was powered by
one 3435 shp turbine engine. The AH-56 had a top speed of 214 knots, a cruise speed of 197 knots, a service ceiling of 26,000 feet, a maxium range of
547 nautical miles, and could climb at 3,420 feet per minute. The AH-56 was Lockheed's entrance into the program. In the end the AH-56 proved to be
too complicated and there were cost overruns. The Army decided to pick the AH-64 because of its simpler fire control and navgation systems.
AH-56
YAH-64(protoype AH-64)
AH-64D
So the question is, Do you think the AH-56 should of entered service instead of the AH-64 given the info here?
I await your replies.