Yep, helicopters are inherently unstable. Stability has been discussed here before, so in a nutshell: Positive stability is the tendency to experience lessening oscillations after a disruption until the aircraft returns to its stable state. Neutral stability is the tendency for the aircraft to maintain its new equilibrium. Negative stability is the tendency for the oscillations after a disruption to grow larger. Many of us built free-flight model aircraft. These have positive stability that allows them to fly without intervention and, given a suitable area, to land unaided. Most GA aircraft are similar. By contrast, a helicopter requires constant, minute control inputs in order to fly. Their inherent instability is what makes them so maneuverable, much like moder jet fighters are very maneuverable but require computers as in interface between the pilot and the controls.
Okay, backpack helicopters. There are several single-seat helicopter designs. Most have little in the way of reserve power. It’s been pointed out to me on these boards that the Mini-500’s engine is working far harder than it was designed to, resulting in failures. So you need an engine powerful enough to swing the rotor system without working so hard that it fails. In addition to the engine you need a transmission. You also need swashplates so that you can vary the pitch of the rotor blades collectively and cyclicly. And the transmission needs a freewheeling unit, by the way, in case of an engine failure. Things are starting to get heavy.
Now how do you counteract torque? There are a couple of ways. The most common is to have an anti-torque rotor. Another way is to have contrarotating rotors on the same shaft, or with twin rotors rotating in opposite directions. Another way is to use tip jets, so you only have to counteract friction – which may be do-able with a fin.
The Hiller HJ-1 Hornet was incredibly noisy under power and had an unacceptable sink rate in autorotation. And I doubt a ramjet-powered backpack helicopter would have enough fuel for useful flights. Twin-blade helicopters need to be fairly large compared to a single-rotor system. Too big for a backpack heli. Kaman makes a twin rotor where the rotor blades intermesh. But since they are inclined to the sides, they’d have to be on high masts for them to work on a backpack and provide enough ground clearance at the tips.
The wiki illustration (I admit I haven’t read the article) has contrarotating rotors to counteract torque. Okay. As long as the pilot doesn’t stumble, the blades won’t hit the ground. Some sort of landing frame would be in order.
And there’s the trusty tail rotor. This is by far the most popular configuration.
But with a tail rotor you need a tail boom. If you have a tail boom, you need a counterweight in front of the rotor mast to balance the structure. A ‘backpack’ helicopter in this configuration may end up looking like a pantomime horse!
So:
[ul][li]Tail rotor design ends up looking like a regular helicopter;[/li][li]Tip-jet design is too noisy and requires too much fuel, plus it needs a fin/rudder;[/li][li]Twin-rotor design needs a wide structure to separate the blades, or a tall structure to prevent the tips of intermeshing blades from hitting the ground. Looking more like another version of the pantomime horse.[/ul][/li]All of the above make one ask, ‘What’s the point?’ If you’re going to have a structure, why not a proper one? But what about the contrarotating design? It seems to me (and I’m not an aeronautical engineer) that it might work. If you could get a powerplant that’s small enough and light enough and powerful enough to spin 15 or 20 feet of rotor at such a speed that will alow them to lift themselves and the transmission with freewheeling unit and swashplates and control linkages and fuel tank and pilot. Oh, and a support structure so that the pilot doesn’t have to carry the whole weight on his shoulders. Landings would of course have to be zero froward speed to reduce the chance of tripping.
So I don’t see ‘backpack helicopters’ being at all practical. You either have to have an airframe anyway, or you won’t be able to get a strong reliable engine that a man can carry on his back.
Tangentally, there was also the Hiller VZ-1 Pawnee – sort of a Dick Tracy flying platform. The third generation one had a seat and helicopter controls (the first two were operated by a standing pilot who shifted his weight to steer) and apparently flew well enough. But they were too small and slow for military use.