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2. Williams X-Jet - Wikipedia

   en.wikipedia.org/wiki/Williams_X-Jet

   Data from General characteristics Crew: 1 Length: 3 ft (0.91 m) approx. Height: 4 ft 0 in (1.22 m) Empty weight: 401 lb (182 kg) Gross weight: 550 lb (249 kg) Powerplant: 1 × Williams F107 turbofan engine, 570 lbf (2.5 kN) thrust (modified) Performance Maximum speed: 52 kn (60 mph, 96 km/h) Endurance: 30–45 minutes Service ceiling: 10,000 ft (3,000 m) Thrust/weight: 1.11 See also Aircraft ...

3. Northrop M2-F2 - Wikipedia

   en.wikipedia.org/wiki/Northrop_M2-F2

   Data from General characteristics Crew: 1 Length: 22 ft 2 in (6.76 m) Wingspan: 9 ft 8 in (2.95 m) Height: 9 ft 6 in (2.90 m) Wing area: 160 sq ft (15 m 2) Empty weight: 4,620 lb (2,096 kg) Gross weight: 6,000 lb (2,722 kg) Max takeoff weight: 7,485 lb (3,395 kg) Powerplant: 1 × Reaction Motors XLR-11 liquid-fuelled rocket motor, 8,000 lbf (36 kN) thrust with four combustion chamber/nozzle ...

4. Boeing Vertol XCH-62 - Wikipedia

   en.wikipedia.org/wiki/Boeing_Vertol_XCH-62

   The rotorcraft was designed to lift a standard Department of Defense, 8 ft × 8 ft × 20 ft (2.4 m × 2.4 m × 6.1 m) MILVAN container weighing up to 22.4 short tons (20,300 kg). [15] Its widely spaced landing gear would allow it to straddle heavy cargoes such as armored vehicles, and still carry twelve troops in its slender fuselage.

5. Wing loading - Wikipedia

   en.wikipedia.org/wiki/Wing_loading

   The Boeing 367-80 airliner prototype could be rolled at low altitudes with a wing loading of 387 kg/m 2 (79 lb/sq ft) at maximum weight. Like any body in circular motion , an aircraft that is fast and strong enough to maintain level flight at speed v in a circle of radius R accelerates towards the center at v 2 / R {\displaystyle v^{2}/R} .

6. Sikorsky CH-53E Super Stallion - Wikipedia

   en.wikipedia.org/wiki/Sikorsky_CH-53E_Super_Stallion

   YCH-53E testing showed that it could lift 17.8 short tons (16.1 t) (to a 50-foot (15 m) wheel height), and without an external load, could reach 170 knots (310 km/h) at a 56,000 lb (25 t) gross weight. This led to two preproduction aircraft and a static test article being ordered.

7. Yakovlev Yak-30 (1960) - Wikipedia

   en.wikipedia.org/wiki/Yakovlev_Yak-30_(1960)

   Data from Wings of Motherland General characteristics Crew: 2 Length: 10.14 m (33 ft 3 in) Wingspan: 9.38 m (30 ft 9 in) Height: 3.4 m (11 ft 2 in) Wing area: 14.3 m 2 (154 sq ft) Airfoil: TsAGI S-9S Empty weight: 1,555 kg (3,428 lb) Gross weight: 2,250 kg (4,960 lb) Max takeoff weight: 2,550 kg (5,622 lb) Fuel capacity: 500 kg (1,100 lb) Powerplant: 1 × Tumansky RU-19-300 turbojet engine, 10 ...