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If you haven't
already done so
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society or require general information please contact ASTRA
using the following Email address: Should you encounter any problems
with this Web
Page please
email: The table below gives a brief
description of the history of the X-Planes from X -1 to X
-44. To access information on any
particular Model simply click on the desired model
number. Alternately visit the full table
below and simply scroll down the list of models. To move to
the top of the full table of models click
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Please note - This table is still under construction, parts of the table are still to be entered.
Index Investigate flight
beyond the sound barrier. First manned aircraft to
achieve supersonic flight on October 14th
1947. Investigating flight
behaviour beyond the speeds of sound, including and
exceeding twice the speed of sound. Speeds to mach 2.44
achieved and flight behaviour examined and coupling
encountered. Investigating flight
behaviour beyond the speeds of sound, including and
exceeding twice the speed of sound. Speeds to mach 2.44
achieved and flight behaviour examined and coupling
encountered. Investigating flight
behaviour beyond the speeds of sound, including and
exceeding twice the speed of sound. Speeds to mach 2.44
achieved and flight behaviour examined and coupling
encountered. Investigating flight
behaviour beyond the speeds of sound, including and
exceeding twice the speed of sound. Speeds to mach 2.44
achieved and flight behaviour examined and coupling
encountered. Investigated performance
of improvements to the thin wing. Achieved supersonic
flight with a 4% thickness/chord wing. Investigated flight with
swept wing as well as aerodynamic heating. Research into high
aerodynamic fiction above mach 2.5, as well as pioneering
the use of steel alloys. Investigated high speed
flight at sustained Mach 2. Poor performance due to
low engine power. Investigated
Semi-tailless aircraft at transonic speeds. Research showed
conventional, semi-tailless, swept wing aircraft not suited
for transonic flight. Investigated variable
swept-wing geometry between 20 degrees amd 60
degrees. Design based upon the
Messerschmitt P.1101 &endash; which lead to the F-111
(General Dynamics) and F-14 (Grumman). Investigated nuclear
propulsion. Neither of the two X-6's
completed before the project was cancelled. A b-36 was used
as a shielded testbed. Used as a
supersonic/hypersonic ramjet testbed. Established database
used for current ramjet/scramjet work. It was the first M-3
air-breathing testbed. Used as a
supersonic/hypersonic ramjet testbed. Established database
used for current ramjet/scramjet work. It was the first M-3
air-breathing testbed. Used as Inexpensive
research vehicle/sounding rocket. Originally a successor
to the captured German V-2s which had been used to
investigate high-altitude payloads. Testbed version of Bell
GAM-63 Rascal air-to-surface missile. Demonstrated that air-to
&endash;surface missiles could be launched and controlled
from heavy bombers. Testbed for SM-64 Navajo
cruise missile. Investigated and proved
aerodynamics of Navajo missile as well as becoming world's
first Mach 2 capable target drone. Testbed for XB-65 Atlas
ICBM ballistic missile. Tested hardware and its
performance. One and a half stage
test vehicle for Atlas ICBM. First full Atlas
configuration flown in November 1958 with a mission range of
6,325 miles. Investigating
"tailsitter" VTOL configuration. Confirmed jet-powered
VTOL flight. Investigating
vectored-thrust VTOL configuration. Data received from this
project used in the design of Hawker P.1127. Investigating hypersonic
flight with speeds beyond mach 6 and heights of over 250,000
feet. Obtained huge database
of hypersonic flight together with unofficial speed record
of Mach 6.7 More
Information - Click
Here Reconnaissance aircraft
disguised as an X-plane for secrecy. 1952 Project cancelled
&endash; experience, data and some hardware later used for
Lockhead U-2 Spy-plane. Multi-stage rocket used
in the investigation of re-entry vehicles. Project created database
for re-entry vehicle design used within the Atlas and Titan
ICBMs. Investigating large
tilt-wing V/STOL aircraft. Used in the design of
Vought XC-142 tilt wing aircraft. Investigation tilt-prop
VTOL design. Confirmed dual-tandem
tilt &endash;prop concept. Piloted vehicle for
hypersonic/orbital research. Project cancelled
&endash; experience and data of materials from this project
contributed to database used for Space Shuttle development.
More
Information - Click
Here Testbed for boundary
layer investigations. Modified Douglas WB-660s
confirmed that laminar flow control
effective. Investigations into
dual-tandem ducted propeller V/STOL aircraft. Confirmed stability for
pitch/roll/yaw and thrust control. (No2 flying at Calspan in
1980s). Investigating
configuration, control & materials for hypersonic
lifting-body re-entry vehicle. Confirmed manoeuvrable
re-entry vehicle as well as new ablative materials later
used on the Shuttle and the X-38. Investigated lift:drag
and controllability issues. Confirmed lifting-body
design for hypersonic/trans-atmosphere
vehicles. Investigating
unpowered/powered gryo-glinder used by crew abandoning
aircraft. Confirmed viability of
"gyro-chute" escape concept for aircraft
crew. Powered sailplane
modified for stealth intelligence gathering
purposes. YO-3A used in Vietnam
designed from X-26B/QT-2 &endash; some details still
classified. Lightweight fighter
prototype based on CL-1200 Lancer. Project terminated
&endash; intended as international F-104
replacement. Investigating single
seated seaplane for police patrols. Pereira 1, selected from
six designs for US Navy's Air Skimmer
Project. Investigating thin,
supercritical-section forward swept wing, close coupled
canard, variable camber with relaxed
stability. Confirmed controlled
flight at high angle-of-attack, vortex flow control and
aeroelastic tailoring preventing divergence. Single-stage-to-orbit
demonstrator for the National AeroSpace Plane
(NASP). Project cancelled
&endash; succeeded by Hyper-X (X-43) of the hypersonic
experimental vehicle programme. More
Information - Click
Here More
Information - Click
Here More
Information - Click
Here
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Website Author: Nick Portwin (portwin@easynet.co.uk)
© 1998 - The material contained within this Web page is copyrighted by ASTRA on behalf of a number of individuals who have contributed to this website.
The material within this website may be reproduced for educational none-profit making purposes. The only condition imposed for reproducing this material is that you acknowledge the source of the material. This acknowledgement should include ASTRA's website address (www.astra.org.uk) as well as ASTRA's email address (info@astra.org.uk).
Date Last Modified: 31 07 1999