Puneet Varma (Editor)

Lockheed X 7

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Top speed
  
4,640 km/h

Length
  
9.98 m

Manufacturer
  
Wingspan
  
3.66 m

Retired
  
1960


The Lockheed X-7 (dubbed the "Flying Stove Pipe") was an American unmanned test bed of the 1950s for ramjet engines and missile guidance technology. It was the basis for the later Lockheed AQM-60 Kingfisher, a system used to test American air defenses against nuclear missile attack.

Contents

Lockheed X-7 Lockheed X7 Specifications A photo

The aircraft is one of the lesser known designs by Kelly Johnson, who went on to become the creator of the SR-71 family of aircraft.

Lockheed X-7 Lockheed X7 Wikipedia

Design and development

Lockheed X-7 Lockheed X7 Specifications A photo

The X-7 was carried aloft by a B-29 or B-50 Superfortress carrier aircraft. A booster ignited after launch and propelled the vehicle to a speed of 1,000 mph (1,625 km/h). The booster was then jettisoned, and the underslung ramjet took over from that point. The X-7 eventually returned to Earth, its descent slowed by multistage parachute. It descended in a vertical nose-down attitude. The nose was a long spike which penetrated the ground upon impact preventing damage to the rest of the airframe.

Lockheed X-7 Lockheed X7 Flying Stove Pipe

A maximum speed of 2,881 miles per hour (4,637 km/h), or Mach 4.31, was attained, setting a record for fastest air-breathing aircraft at the time. A total of 130 X-7 flights were conducted from April 1951 to July 1960.

The X-7 was unique in that it was constructed of steel, as opposed to the titanium used on later ramjets such as the more well known SR-71, and its predecessors, the A-12 and YF-12. The X-2 test aircraft preceded the X-7 by having Stainless steel wings, but its fuselage was composed of Nickel alloy. Steel was not widely used in aircraft until the later Mig-25 Foxbat.

The X-7 was also used to test HEF-2 and Hi Cal-3 zip fuel, which has a superior heating value of 26,500 Btu/lb. compared to hydrocarbon fuel with 18,400 Btu/lb.

Specifications (X-7A-1)

General characteristics

  • Crew: None
  • Length: 32 ft 9 in (9.98 m)
  • Wingspan: 12 ft (3.66 m)
  • Height: 7 ft (2.1 m)
  • Loaded weight: 8,000 lb (3,600 kg)
  • Powerplant:
  • 1 × Allegany Ballistics Laboratory X202-C3 solid-fuel rocket, 105,000 lbf (467 kN)
  • 1 × various Marquardt MA20 ramjets under test, ()
  • Performance

  • Maximum speed: Mach 4.31 (2,881 mph, 4,640 km/h)
  • Service ceiling: 106,000 ft (32,317 m)
  • The A-3 variant was longer and narrower.

    References

    Lockheed X-7 Wikipedia