2026-07-08
In November 1953, a spindly contraption made of welded steel tube, a Bell Model 47 helicopter cockpit bubble, and two Fairchild J44 turbojets mounted on trunnions lifted off the ground at Niagara Falls Airport. It hovered. It transitioned into forward flight. It landed. And almost no one remembers it existed.
The Bell Model 65 Air Test Vehicle was the first American aircraft to achieve vectored-thrust jet VTOL flight — six years before the Hawker P.1127 (Harrier prototype) flew, and eight years before the Short SC.1 demonstrated full transition. Its designer, David Forman, working under Bell's chief of preliminary design Kenneth Wernicke, built it on a shoestring: no government contract, no formal program, just Bell's internal R&D budget and a determination to prove that swiveling the engines themselves — rather than deflecting exhaust through nozzles — could work.
The specs are almost comical in their simplicity:
1,000 lbf of thrust, mounted on gimbals that rotated from vertical (lift) to horizontal (cruise)So why don't you know about it? Three reasons:
1. Thrust-to-weight was brutal. Two J44s at 1,000 lbf each gave 2,000 lbf total thrust against a 2,000 lb airframe — a T/W ratio of barely 1.0 with no payload, no fuel margin, and no pilot. Every hover was a knife-edge exercise. The J44 was a target-drone engine; nothing more powerful was small enough to fit.
2. Bell had a bigger horse in the race. The company was already deep into the XV-3 tiltrotor program (which led directly to the XV-15 and V-22). Management saw jet VTOL as a distraction from Bell's real bet: rotors. Forman's team got cannibalized.
3. The Air Force wasn't buying. In 1954, USAF was fixated on Mach 2 interceptors and strategic bombers. A subsonic testbed proving a hover concept had no procurement pathway. The Model 65 was donated to the Smithsonian in 1955 and sat in storage for 50 years.
Why revisit it now? The Model 65's core insight — rotating the entire engine rather than the exhaust — is exactly what's making the current generation of eVTOL aircraft work. Joby, Archer, and Beta all tilt their propulsors bodily. The reason it failed in 1953 was thrust-to-weight; today's high-bypass turbofans hit T/W of 8:1, and electric ducted fans approach 15:1 at the disk. A modern Model 65 with two Williams FJ44-class engines (3,600 lbf each, 450 lb dry) would have a hover T/W of 3.6 — luxurious. Add fly-by-wire (Forman's pilot was fighting mechanical linkages) and the aircraft becomes trivially controllable.
The Harrier's Pegasus engine cost $400 million to develop across 15 years. Forman built a working proof of the same idea for the cost of two drone engines and a welded frame. The concept was never wrong — it just needed engines that hadn't been invented yet.
