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January 1976
- Mach 3.0, Breaking the Sound Barrier in the Bell X-2
February 1976
- Mach 3.0, Exploring the Edges of Outer Space in the Bell X-2
April 1982
- Behind The Bell X-1 Rocket Plane Crashes
September 1983
- Stiletto, A Detailed Look At Douglas Aircraft’s Needle-Nosed, Supersonic Research Ship, The X-3.
February 1991
- Machbusters, Memoirs Of A Veteran Test Pilot
November 1996
- Rendezvous At Mach 1, Commemorating The Breaking Of The Sound Barrier!
January 1999
- Prototypes: The X-Jobs
June 2002
- “Toward The Unknown”, Filming the 1956 Warner Brothers Classic about the Bell X-2
September 2003
- Father of the Motherships, The Planes that Launched the Legends and the Pilots that Flew Them
September 2004
- Swingin’ on a Spar, the Bell X-5 variable geometry wing
November 2003
- Dueling Test Pilots, Yeager vs. Crossfield
- Salute to “The Right Stuff”
- Back in the Saddle, the story of Pancho Barnes
January 2005
- Bell X-2 Color Schemes
April 2007
- Douglas X-3 Stiletto
Manuals & Photos
- X-1A Pilot’s Handbook 1951
- X-3 Operating Instructions 1951
- X-4 Operating Instructions 1948
- X-5 Research Plane 1954
- American X-Vehicles X-1 to X-50
- Toward Mach 2 – The Douglas D-558 Program
- Probing The Sky, NASA Aeronautics
- Flights of Discovery, 50 Years at NASA Dryden
- And nearly 400 photos of early X-Planes!
Early X-Planes Specifications
Bell X-1
Bell X-1E
Bell X-2
Douglas X-3
Northrop X-4
Bell X-5
Douglas D-558-1
Douglas D-558-2
General Characteristics
- Crew:Â one
- Length:Â 30 ft 11 in (9.4 m)
- Wingspan:Â 28 ft (8.5 m)
- Height:Â 10 ft (3.3 m)
- Wing area: 130 ft² (12 m²)
- Empty weight:Â 7,000 lb (3,175 kg)
- Loaded weight:Â 12,225 lb (5,545 kg)
- Max. takeoff weight:Â 12,250 lb (5,557 kg)
- Powerplant: one × Reaction Motors XLR-11-RM3 liquid-propellant rocket, 6,000 lbf (1,500 lbf per chamber) (26.7 kN) each
- Color : International Orange (same color as the Golden Gate Bridge)
Performance
- Maximum speed:Â 957 mph (Mach 1.26) (1,541 km/h)
- Range:Â five minutes (powered endurance)
- Service ceiling:Â 71,902 ft (21,916 m)
- Wing loading: 94 lb/ft² (463 kg/m²)
- Thrust/weight:Â 0.49
On Display
- X-1-1, Air Force Serial Number 46-062, is currently displayed in the Milestones of Flight gallery of the National Air and Space Museum in Washington, DC, alongside the Spirit of St. Louis and SpaceShipOne.
- X-1B, AF Ser. No. 48-1385, is on display in the Research & Development Hangar at the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Ohio.
General Characteristics
- Crew:Â one
- Length:Â 31 ft (9.4488 m)
- Wingspan:Â 22 ft 10 in (6.9596 m)
- Height:Â 10 ft 10 in (3.3 m)
- Wing area: 115 ft² (10.684 m²)
- Empty weight:Â 6,850 lb (3,107.107 kg)
- Loaded weight:Â 14,750 lb (6,690.487 kg)
- Powerplant: 1 × Reaction Motors RMI LR-8-RM-5 rocket, 6,000 lbf (26.7 kN)
Performance
- Maximum speed:Â 1,450 mph (Mach 2.24) (2,333.548 km/h)
- Range:Â 4 minutes 45 seconds (powered endurance)
- Service ceiling:Â 90,000+ ft (27,432+ m)
On Display
- X-1E, AF Ser. No. 46-063, is on display in front of the NASA Armstrong Flight Research Center headquarters building at Edwards Air Force Base, California.
General Characteristics
- Crew:Â one, pilot
- Length:Â 37 ft 10 in (11.5 m)
- Wingspan:Â 32 ft 3 in (9.8 m)
- Height:Â 11 ft 10 in (3.6 m)
- Wing area: 260 ft² (24.2 m²)
- Airfoil:Â 2S-50 bicon
- Empty weight:Â 12,375 lb (5,600 kg)
- Loaded weight:Â 24,910 lb (11,300 kg)
- Max. takeoff weight:Â 24,910 lb (11,300 kg)
- Powerplant: 1 × Curtiss-Wright XLR25 rocket engine, 15,000 lbf (67 kN)at sea level
Performance
- Maximum speed:Â Mach 3.196 (2,094 mph, 3,370 km/h)
- Service ceiling:Â 126,200 ft (38,466 m)
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General Characteristics
- Crew:Â one
- Length:Â 66 ft 9 in (20.3 m)
- Wingspan:Â 22 ft 8 in (6.9 m)
- Height:Â 12 ft 6 in (3.8 m)
- Wing area: 166.5 ft² (15.47 m²)
- Empty weight:Â 16,120 lb (7,310 kg)
- Max. takeoff weight:Â 23,840 lb (10,810 kg)
- Powerplant: 2 × Westinghouse J34 afterburning turbojet, 3,370 lbf, 4,850 lbf with afterburning (15.0 kN, 21.6 kN with afterburning) each
Performance
- Maximum speed:Â 700 mph (1,125 km/h)
- Range:Â 497 mi (800 km)
- Service ceiling:Â 38,000 ft (11,600 m)
- Thrust/weight:Â 0.40
On Display
- The sole X-3 was transferred in 1956 to the National Museum of the United States Air Force at Wright-Patterson Air Force Base, Ohio As of 2008 it is on display in the Museum’s Research & Development Gallery.
General Characteristics
- Crew:Â one
- Length:Â 22 ft 3 in (7.09 m)
- Wingspan:Â 26 ft 10 in (8.18 m)
- Height:Â 14 ft 10 in (4.52 m)
- Wing area:Â 200 sq ft (18.6 m2)
- Aspect ratio:Â 3.6:1
- Empty weight:Â 5,507 lb (2,500 kg)
- Max. takeoff weight:Â 7,820 lb (3,550 kg)
- Powerplant: 2 × Westinghouse J30-WE-7/9 turbojet, 1,600 lbf (7.1 kN) each
Performance
- Maximum speed:Â 625 mph (543 knots, 1,006 km/h)
- Range:Â 420 mi (365 nmi, 676 km)
- Service ceiling:Â 42,300 ft (12,900 m)
- Rate of climb:Â 7,700 ft/min (39.1 m/s
General Characteristics
- Crew:Â 1
- Length:Â 33 ft 4 in (10.1 m)
- Wingspan:
- Unswept:Â 33 ft 6 in (10.2 m)
- 60° sweep: 20 ft 10 in (6.5 m)
- Height:Â 12 ft (3.6 m)
- Wing area: 175 sq. ft. (16.26 m².)
- Empty weight:Â 6,336 lb (2,880 kg)
- Max. takeoff weight:Â 9,980 lb (4,536 kg)
- Powerplant: 1 × Allison J35-A-17 turbojet, 4,900 lbf (21.8 kN)
Performance
- Maximum speed:Â 716 mph (1,150 km/h)
- Range:Â 750 mi (1,207 km)
- Service ceiling:Â 49,900 ft (15,200 m)
- Thrust/weight:Â 0.50:1
On Display
- The sole surviving X-5 is now at the National Museum of the United States Air Force at Wright-Patterson Air Force Basenear Dayton, Ohio. It was delivered to the Museum in March 1958. It is displayed in the Museum’s Research & Development Hangar.
General Characteristics
- Crew: one pilot
- Payload: 500 lb of instruments (227 kg)
- Length: 35 ft 8 in (10.87 m)
- Wingspan: 25 ft 0 in (7.62 m)
- Height: 12 ft 1 in (3.68 m)
- Wing area: 150.7 ft² (14.00 m²)
- Loaded weight: 9,750 lb (4,423 kg)
- Max. takeoff weight: 10,105 lb (4,583 kg)
- Powerplant: 1 × Allison J35-A-11 turbojet, 5,000 lbf (22 kN)
Performance
- Maximum speed: 650 mph at sea level (1,050 km/h)
- Stall speed: 137 mph (221 km/h)
- Service ceiling: 45,700 ft (13,900 m)
- Rate of climb: 9,220 ft/min (2,810 m/min)
- Wing loading: 67 lb/ft² (330 kg/m²)
- Thrust/weight: 0.51
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General Characteristics
- Crew: one pilot
- Length: 42 ft 0 in (12.8 m)
- Wingspan: 25 ft 0 in (7.6 m)
- Height: 22 ft 8 in (3.8 m)
- Wing area: 175 ft² (16.2 m²)
- Empty weight: 9,421 lb (4,273 kg)
- Max. takeoff weight: 15,266 lb (6,923 kg)
- Powerplant:
- 1 × Westinghouse J34-WE-40 turbojet, 3,000 lbf (13 kN)
- 1 × Reaction Motors XLR-8-RM-5 rocket engine, 6,000 lbf (27 kN)
Performance
- Maximum speed: 720 mph, 1,250 mph when air-launched (1,160 km/h, 2,010 km/h when air-launched)
- Stall speed: 160.1 mph (257.7 km/h)
- Service ceiling: 16,500 ft (5,030 m)
- Rate of climb: 22,400 ft/min, 11,100 ft/min under rocket power only (6,830 m/min., 3,380 m/min under rocket power only)
- Wing loading: 87.2 lb/ft² (426 kg/m²)
- Thrust/weight (jet): 0.39