In the early 1960s, a boxy little jet rose slowly off the ground at a Lockheed test site in Georgia, hung in the air, and set down again. On the face of it, the Lockheed XV-4 Hummingbird had done the impossible-looking thing: vertical take-off on ordinary jet engines. In reality it was clawing its way into the air with almost nothing to spare — and the clever idea at its heart never delivered what its designers promised.
The Hummingbird is one of aviation’s great “free lunch” stories: a physics trick that looked like a way to get lift for nothing, and quietly refused to work.
Aircraft: Lockheed XV-4 Hummingbird (originally VZ-10)
Operator: US Army research programme, built by Lockheed-Georgia
Idea: “Ejector augmenter” VTOL — jet exhaust dragging in extra air to multiply lift
Reality: Thrust-to-weight of just 1.04 — it could barely lift itself
Built: Two aircraft; both crashed (XV-4A in 1964, fatally; XV-4B in 1969)
Result: Concept judged not competitive; programme abandoned
The free-lunch idea
Lockheed had been studying jet ejectors since the mid-1950s, and in 1961 won a US Army contract to build two research aircraft to prove the concept. The idea was elegant. Instead of pointing the engine exhaust straight down — brute-force lift that burns enormous fuel — you feed it through carefully shaped ejector ducts inside the fuselage. The fast jet exhaust drags in a much larger mass of ambient air, and the mixed flow, in theory, produces far more lift than the raw exhaust alone.
The Hummingbird carried two Pratt & Whitney JT12 turbojets along its flanks. Diverter valves could send their exhaust aft for normal flight, or down through the ejector chambers in the belly for hovering. The design target was a thrust augmentation of 1.4 — a 40 percent free boost. That was the whole point of the aircraft.

The number that killed it: 1.04
The physics did not cooperate. When the real aircraft was tested, the ejector augmentation came out far below the promise — and the numbers were brutal. After installation losses, the Hummingbird managed a thrust-to-weight ratio of just 1.04. In other words, it could lift its own weight and almost nothing else. There was no margin for fuel, payload, or error.
That marginal lift did not just make the aircraft useless as a vehicle; it crippled the research programme itself, because there was no spare performance to explore.
Two aircraft, two crashes
The first XV-4A flew conventionally in July 1962, made its first free hover in May 1963, and completed the tricky transition between vertical and forward flight that November. Then, on 10 June 1964, it crashed, killing its pilot.
Lockheed did not give up. It rebuilt the surviving airframe as the XV-4B, throwing out the ejector trick entirely and fitting six small General Electric J85 engines — four of them pointing straight down as dedicated lift jets, the honest brute-force approach. That aircraft crashed too, in Georgia in 1969; this time the pilot, Harlan Quamme, ejected safely. With both machines gone, the programme was abandoned.

The idea that would not die
The strange thing is that the ejector-augmenter concept kept seducing engineers for years afterward. Its most famous descendant, the Rockwell XFV-12A, chased the same free-lunch lift a decade later and did even worse, managing an augmentation of barely 1.1 — so little that it never flew freely at all.
In the end it was the honest approaches that won: direct-lift jets and, above all, the vectored thrust of the Harrier. The Hummingbird is a reminder that in aviation, when a design promises something for nothing, the something usually turns out to be the aircraft itself.
Sources: GlobalSecurity.org (XV-4 flight-test evaluation); Wikipedia; NASA Ames; autoevolution.




0 Comments