X-Planes Experimental Aircraft
The unknown is inherently unpredictable. Wind tunnels, simulators and computers can only model what is known. That became clear by the mid-1940s as engineers began to probe the technological challenges of piloted, supersonic flight. By early 1945 the world's first experimental airplanes were under development: the rocket-powered XS-1 (later designated X-1), built under Army sponsorship by Bell Aircraft, and the turbojet-powered D-558-1 constructed by Douglas Aircraft under Navy patronage. With the supersonic X-1, flight testing assumed a distinctive process using highly experimental research programs -- such as with the X-3, X-4, X-5, and through dozens of subsequent X-series aircraft.
Research aircraft are the tools for exploration and discovery. Each is instrumented to acquire data about the aircraft, its systems and even the surrounding environment during research flights. These are typically flown by the Air Force in conjunction with NASA and conducted in a very methodical fashion to answer largely theoretical questions concerning innovative aircraft design principles. The X-15 explored hypersonic and exoatmospheric flight. Indeed, within an eight-month span in 1961, it became the first aircraft to exceed Mach 4, -5, and -6, and it later went on to become the first--and, so far, only--airplane to fly in near space as it soared to a peak altitude of more than 67 miles (354,200 feet).
Until the 1970s, experimental planes (designated "X"-planes for "experimental") were the chief research tools for flight regimes that wind tunnels, simulators and production aircraft
could not approach.
The X-Plane Program has evolved from being the first rocket-powered airplane to break the sound barrier (the X-1 on 14 October 1947) and included over 30 different major research designs, although not all were developed into flying prototypes . As the program progressed, other non-rocket-powered experimental aircraft were built and tested. These aircraft included: a range of vertical takeoff and horizontal landing vehicles; smaller, propeller-driven reconnaissance vehicles; and a series of unmanned missile testbeds of both single and multistage designs. Although the program grew to include conventional propeller-driven aircraft, all designs had in common the
aspect of being highly valuable research tools for advancement of aerodynamics and astronautics.
Accomplishments of the X-Plane family have been many. The program included: (1) the first aircraft to break the sound barrier; (2) the first aircraft to use a variable-sweep-wing in flight; (3) the first to fly at altitudes in excess of 30,000, 60,000, and 90,000 m (100,000, 200,000 and 300,000ハft); (4) the first to use exotic alloy metals for primary structure; (5) the first to test gimbaled jet and rocket engines; (6) the first to use jet-thrust for launch and landing; (7) the first to fly three, four, five, and six times the speed of sound; (8) the first to test boundary-layer-airflow control theories over an entire wing at transonic speeds; (9) the first to successfully
complete a 180-degree turn using a post-stall maneuver; and (10) the first missile to reach an intercontinental flight range.
Another member of the X-Plane Program would be the X-33. As a reusable spaceplane, the X-33 continues the research line developed by various components of the X-Program, such as the X-10 which tested cruise missile components; the X-12, the Atlas B missile which tested one-and-one-half propulsion staging and obtained the first intercontinental flight distance for a US missile; the X-15 which explored the problems of space and reentry at high speeds (Mach 6) and altitudes; the X-17 which explored high Mach effects on reentry vehicles; and the X-23A which was the first maneuvering lifting reentry vehicle. The X-17 was a multistage rocket design which transported various reentry vehicle configurations to very high altitudes to examine their reentry
characteristics. The X-23A was launched by a modified intercontinental ballistic missile and utilized a 斗ifting body? design to glide back to earth. Information acquired from the X-23A was instrumental in later development of the Space Shuttle.
The majority of testing for the X-Plane family has occurred at Edwards Air Force Base (formerly known as Muroc Army Airfield). Hosts within Edwards include the Air Force Flight Test Center and Dryden Flight Research Center. Other sites which have served as X-Plane testing sites include: Langley Research Center and Ames Research Center; various Government owned ships; White Sands Missile Range, New Mexico; Wright-Patterson Air Force Base, Ohio; Cape Canaveral Air Station, Florida; Pinecastle Air Force Base, Florida; Buffalo, New York; and the National Aviation Facilities Experimental Center in Atlantic City, New Jersey. Edwards has seen more X-Plane programs and test flights than any other similar facility in the US.
As with every research program testing prototype equipment, the X-Plane Program has not been without technical glitches and equipment failures. Since the beginning of the program痴 manned flight operations in 1946, approximately 15 major accidents and 4 fatalities (pilots) have been associated with manned vehicle tests. Three of these fatalities were from the X-2 Program, flown between 1952 and 1956, and the remaining fatality happened in 1967 during an X-15 research flight. Stringent range safety controls have resulted in no civilian property damage losses or fatalities being reported as a result of any X-Plane Program accident. Given the overwhelming
number of test flights, the small number of accidents which resulted in loss of aircraft or life can be considered a remarkable program achievement.
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
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
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
X- 1B
Bell Aircraft
1
1954- 58
27
Edwards AFB
Exploratory aerodynamic
heating tests; experimental
reaction control system
First reaction
controlled flight
X- 1D
Bell Aircraft
1
1951
1
Edwards AFB
Continue X- 1 goals at
higher speeds and altitudes
No major milestones, Explosion during
captive flight;
vehicle jettisoned
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
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
Gasket explosion
destroyed first X- 2;
second aircraft lost
to inertial coupling
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
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
X- 5
Bell Aircraft
2
1952- 55
133
Edwards AFB
Investigate aerodynamics
of variable- seep- wing
design
Successful sweep- wing
operation
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
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
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
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
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
X- 11 (unmanned)
Convair
Astronautics
Division
8
1956- 58
8 Cape
Canaveral
Provide flight data for Atlas
missile
First ICBM prototypes
X- 12
(unmanned)
Convair
Astronautics
Division
5
1958
5
Cape
Canaveral
Test propulsion- staging
guidance system, nose
reentry configuration
First intercontinental
range mission of 6,325
miles
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
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
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 hyper-
sonic flight vehicle;
altitude of 354,200 ft
obtained; Mach 6.7
reached
4 Mid- flight explosions
(2); loss of control
(1); collapsed
landing gear (1)
X- 16 Bell Aircraft
Canceled
None
None
None
None
High- altitude, long- range
reconnaissance aircraft
X- 17
(unmanned)
Lockheed Missiles
26
1955- 57
26
Holloman AFB
Explore reentry
characteristics
High Mach effects on
reentry vehicles
X- 18
Hiller Aircraft
1
1959- 61
20
Edwards AFB
Explore large VTOL
vehicles
First tilt- wing usage for
VTOL
X- 19
Curtiss- Wright
2
1964- 65
50
Caldwell;
NAFEC, NJ
Test VTOL technology
using radial lift
Dual- tandem tilt
propeller use
One Equipment failure
X- 20
Boeing
Canceled
None
None
None
Piloted orbital flight Provided heat materials
testing
X- 21A
Northrop
Corporation
2
1963- 64
Unknown
Edwards AFB
Test full- scale boundary
control on large aircraft
Proved Laminar Flow
Control viable
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; One hydraulic system
failure
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
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 trans-
atmospheric aircraft
X- 25,
X- 25A,
X- 25B
Bensen Aircraft
3
1968
None
Raleigh, NC
Test discretionary descent
vehicle designs
Insight on pilot training
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
X- 27
Lockheed-
California
Canceled
None
None
None
Advanced, lightweight
fighter
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
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
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
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
Failure of the pitot ?
static system:
erroneous total
pressure data
X-32
X-33
Lockheed- Martin
Skunk Works
1
1999-2000
15
Edwards AFB
Develop reusable single-
stage- to- orbit transportation
vehicle
X-34
X-35
X-36
X-37
X-38
X-39
X-40
X-41
X-42
X-43
X-44
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
Sources and Resources
http://www.fas.org/man/dod-101/sys/ac/x.htm
Maintained by Robert Sherman
Originally created by John Pike
Updated Sunday, March 14, 1999 5:09:16 AM