Summary of the X-Plane Program.
|
Model
|
Manufacturer
|
No. of Vehicles Built
|
Years of Operation
|
No. of Flights
|
Primary Testing Facility
|
Research Goals
|
Program Achievements
|
No. of
Major Accidents
|
Causes of Accidents
|
No. of Fatalities
|
Civilian Involvement
|
X-1 |
Bell Aircraft |
3
|
1946-51
|
157
|
Edwards AFB |
Investigate flight characteristics
at greater than sonic velocities. Structural, physiological phenomena within
transonic speed envelope |
First Mach 1+ flight; Maximum
altitude of 71,902 ft |
1
|
Defueling Explosion |
0
|
None |
X-1A |
Bell Aircraft |
1
|
1953-55
|
25
|
Edwards AFB |
Continue X-1 goals at higher speeds
and altitudes |
Obtained speed of Mach 2.44; Maximum
altitude of 90,440 ft |
1
|
Explosion during captive flight;
vehicle jettisoned |
0
|
None |
X-1B |
Bell Aircraft |
1
|
1954-58
|
27
|
Edwards AFB |
Exploratory aerodynamic heating
tests; experimental reaction control system |
First reaction controlled flight |
0
|
Not applicable |
Not applicable |
Not applicable |
X-1D |
Bell Aircraft |
1
|
1951
|
1
|
Edwards AFB |
Continue X-1 goals at higher speeds
and altitudes |
No major milestones |
1
|
Explosion during captive flight;
vehicle jettisoned |
0
|
None |
X-1E |
Bell Aircraft, Stanley Aircraft
(wings) |
1
|
1955-58
|
26
|
Edwards AFB |
High-speed wing performance |
Mach 2.24, altitude 73,458 ft;
first flight with ventral fins |
0
|
Not applicable |
Not applicable |
Not applicable |
X-2 |
Bell Aircraft |
2
|
1952-56
|
20
|
Edwards AFB |
Swept-wing performance; higher
speeds and altitude than X-1 |
New altitude record of 126,200
ft; new speed record of Mach 2.87 |
2
|
Gasket explosion destroys first
X-2; second aircraft lost to inertial coupling |
3
|
None |
X-3 |
Douglas Aircraft |
1
|
1954-56
|
20
|
Edwards AFB |
High speed aerodynamic phenomenon;
titanium construction; take off, land under its own power |
Led to understanding of inertia
coupling |
0
|
Not applicable |
Not applicable |
Not applicable |
X-4 |
Northrop Aircraft |
2
|
1950-53
|
82
|
Edwards AFB |
Test tailless, semi-tailless configuration
at transonic speeds |
Showed tailless craft not suited
for transonic flight |
0
|
Not applicable |
Not applicable |
Not applicable |
X-5 |
Bell Aircraft |
2
|
1952-55
|
133
|
Edwards AFB |
Investigate aerodynamics of variable-seep-wing
design |
Successful sweep-wing operation |
0
|
Not applicable |
Not applicable |
Not applicable |
X-6 |
Convair Division, General Dynamics |
1 shield-test aircraft (modified B-36H)
|
1955-57
|
47
|
Convair Testing Facility |
Test feasibility of nuclear propulsion |
Program terminated before prototypes
constructed |
0
|
Not applicable |
Not applicable |
Not applicable |
X-7A, X-7A-3, X-7B, X-Q5 (unmanned) |
Lockheed Missiles |
61
|
1951-60
|
130
|
New Mexico |
Test viability of ramjet engines
for anti-aircraft missiles; modified to testing of powerplants |
Obtained Mach 4.31, first air-breathing
full-scale research aircraft designed as Mach 3 testbed |
0
|
Not applicable |
Not applicable |
Not applicable |
X-8A, X-8B, X-8C, X-8D Aerobees
(unmanned) |
Aerojet Engineering |
108 (X-8 designation) 800+ (Aerobees)
|
1947-56
|
Unknown
|
White Sands, Holloman AFB |
Upper air research, parachute
recovery system |
Peak altitude of 121 miles |
0
|
Not applicable |
Not applicable |
Not applicable |
X-9 (unmanned) |
Bell Aircraft |
31
|
1949-53
|
28
|
Holloman AFB |
Test air-to-surface missiles;
guidance systems, etc. |
First chemical warhead test vehicle
to test supersonic clusterable dispersion |
9 unsuccessful flights
|
Servo system failures |
0
|
Not applicable |
X-10 (unmanned) |
North American Aviation |
13
|
1955-59
|
15
|
Edwards AFB |
Testbed for cruise missile components |
Established technology base for
remote control; first Mach 2-capable target drone |
3 unsuccessful flights
|
Communications disruption; miswiring;
autopilot malfunction |
0
|
Not applicable |
X-11 (unmanned) |
Convair Astronautics Division |
8
|
1956-58
|
8
|
Cape Canaveral |
Provide flight data for Atlas
missile |
First ICBM prototypes |
0
|
Not applicable |
Not applicable |
Not applicable |
X-12 (unmanned) |
Convair Astronautics Division |
5
|
1958
|
5
|
Cape Canaveral |
Test 1½-propulsion-staging
guidance system, nose reentry configuration |
First intercontinental range mission
of 6,325 miles |
0
|
Not applicable |
Not applicable |
Not applicable |
X-13 |
Ryan Aeronautical Company |
2
|
1955-57
|
Unknown
|
Edwards AFB |
Test pure-jet vertical takeoff
and landing |
First successful VTOL flight on
jet thrust alone |
0
|
Not applicable |
Not applicable |
Not applicable |
X-14, X-14A, X-14B |
Bell Aircraft |
1
|
1957-81
|
Unknown
|
Moffet Field |
Test VTOL technology |
First VTOL aircraft using jet
thrust diverter system for vertical lift |
0
|
Not applicable |
Not applicable |
Not applicable |
X-15, X-15A-2 |
North American Aviation |
3
|
1959-68
|
199
|
X-15 High Range (Wendover, UT,
to Edwards AFB) |
Explore problems of space and
atmospheric flight at very high speeds and altitudes |
First manned hypersonic flight
vehicle; altitude of 354,200 ft obtained; Mach 6.33 reached |
4
|
Mid-flight explosions (2); loss
of control (1); collapsed landing gear (1) |
1
|
Not applicable |
X-16 |
Bell Aircraft |
Canceled
|
None
|
None
|
None |
High-altitude, long-range reconnaissance
aircraft |
Not applicable |
Not applicable
|
Not applicable |
Not applicable |
Not applicable |
X-17 (unmanned) |
Lockheed Missiles |
26
|
1955-57
|
26
|
Holloman AFB |
Explore reentry characteristics |
High Mach effects on reentry vehicles |
0
|
Not applicable |
Not applicable |
Not applicable |
X-18 |
Hiller Aircraft |
1
|
1959-61
|
20
|
Edwards AFB |
Explore large VTOL vehicles |
First tilt-wing usage for VTOL |
0
|
Not applicable |
Not applicable |
Not applicable |
X-19 |
Curtiss-Wright |
2
|
1964-65
|
50
|
Caldwell; NAFEC, NJ |
Test VTOL technology using radial
lift |
Dual-tandem tilt propeller use |
1
|
Equipment failure |
0
|
Not applicable |
X-20 |
Boeing |
Canceled
|
None
|
None
|
None |
Piloted orbital flight |
Provided heat materials testing |
Not applicable
|
Not applicable |
Not applicable |
Not applicable |
X-21A |
Northrop Corporation |
2
|
1963-64
|
Unknown
|
Edwards AFB |
Test full-scale boundary control
on large aircraft |
Proved Laminar Flow Control viable |
0
|
Not applicable |
Not applicable |
Not applicable |
X-22A |
Bell Aerospace |
2
|
1966-84
|
501
|
Bell, Calspan Test Facilities |
Research dual-tandem-ducted propeller
configuration; research V/STOL handling using variable stability system
design |
Ducted fan viability, advancement
of VTOL technology |
1
|
hydraulic system failure |
0
|
None |
X-23A (unmanned) |
Martin Marietta |
4
|
1966-67
|
3
|
Vandenberg AFB/Pacific Ocean |
Test configurations, control systems,
and ablative materials for hypersonic reentry vehicles |
First maneuverable reentry vehicle |
0
|
Not applicable |
Not applicable |
Not applicable |
X-24A, X-24B |
Martin Marietta |
1
|
1969-75
|
64
|
Edwards AFB |
Research of aerodynamics, flight
characteristics of manned vehicle with FDL-7 configuration |
Verified theoretical advantages
of lifting body configuration for hypersonic transatmospheric aircraft |
0
|
Not applicable |
Not applicable |
Not applicable |
X-25, X-25A, X-25B |
Bensen Aircraft |
3
|
1968
|
|
Raleigh, NC |
Test discretionary descent vehicle
designs |
Insight on pilot training |
0
|
Not applicable |
Not applicable |
Not applicable |
X-26A, X-26B |
Schweizer Aircraft, Lockheed Missiles |
6
|
1967-88
|
Unknown
|
Vietnam |
Develop ultra-quiet surveillance
aircraft |
Use as training vehicle; contributions
to stealth designs |
3
|
Training exercises |
0
|
Not applicable |
X-27 |
Lockheed-California |
Canceled
|
None
|
None
|
None |
Advanced, lightweight fighter |
None |
Not applicable
|
Not applicable |
Not applicable |
Not applicable |
X-28A |
George Pereira, Osprey Aircraft |
1
|
1971
|
Unknown
|
Philadelphia Naval Base, PA |
Explore usefulness of small, single-place
seaplane for civil police patrol in Southeast Asia |
Unique contribution as home-built
aircraft in X-Plane program |
0
|
Not applicable |
Not applicable |
Not applicable |
X-29A |
Grumman Aerospace |
2
|
1984-90
|
Unknown
|
Edwards AFB |
Test forward-swept wing design,
advanced composites, other aerodynamic advances |
First FSW aircraft to fly supersonically
in level flight |
0
|
Not applicable |
Not applicable |
Not applicable |
X-30 |
None selected |
None
|
None
|
None
|
None |
Serve as testbed for sustained
hypersonic speeds within atmosphere or as space vehicles for orbital payload
delivery |
Not applicable |
Not applicable
|
Not applicable |
Not applicable |
Not applicable |
X-31A |
Rockwell International, Deutsche
Aerospace |
2
|
1990-95
|
523
|
Edwards AFB |
Break "stall-barrier," examine
angles of attack |
180 degree turn post-stall maneuver |
1
|
Failure of the pitot ñ static
system: erroneous total pressure data |
0
|
None |
X-33 |
Lockheed-Martin Skunk Works |
None
|
None
|
None
|
None |
Develop reusable single-stage-to-orbit
transportation vehicle |
Not applicable |
Not applicable
|
Not applicable |
Not applicable |
Not applicable |
Key to Acronyms:
AFB = Air Force Base
FDL-7 = Flight
Dynamics Laboratory-7 (a prototype test craft of the Air Force's Flight
Dynamics Laboratory, a predecessor to the X-24B).
FSW = forward swept wing
ICBM = intercontinental ballistic missile
V/STOL = vertical/short takeoff and landing
VTOL = vertical takeoff and landing |