Development of the HFV-3X
Hypersonic Flight
Vehicle

HFV-3X Hypersonic
Aircraft Wind Tunnel Model

HFV-3X Hypersonic
Aircraft
AeroWindTunnel
Wire Frame Design
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Introducing
the HFV-3X, AeroRocket's version of the DARPA HTV-3X known as
the Blackswift represents AeroRocket's proposal for a
new hypersonic spacecraft capable of flight to 300,000
feet and top speed from Mach 5 to Mach 10. A
miniature subsonic wind tunnel model of the
new HFV-3X has been
fabricated for experimental determination of CD,
CL, CLa, CMa
and L/D for use with
AeroWindTunnel
a subsonic and supersonic aircraft design program. Supersonic drag and lift properties of the
HFV-3X design will be investigated using AeroRocket's new shock tube
wind tunnel system.
All AeroRocket software purchasers are eligible to download the latest
HFV-3X design file.
Please use the
AeroRocket Free Download
request
form to receive a username and
password to download this information.
The supplied username
and password will be valid for a limited
time.
On the request form please specify HFV-3X Design
as the requested item for download and be sure the
email address, first name and last name are the same used for ordering AeroRocket software or services
from Emetrix. Please see the
Wikipedia article about the HTV-3X that contains DARPA video
and other interesting information about this proposed space plane.
HFV-3X Design
(348 KB
Download - Password Required):
WinZip file containing techniques used to fabricate the 9 inch long HFV-3X
subsonic wind
tunnel model, HFV-3X wind tunnel model templates, full size
orthographic image of the HFV-3X and an
AeroWindTunnel
screen shot showing CD verses Mach number for the HFV-3X. Must be an
AeroRocket software purchaser. More information
will be included in the download as development of the HFV-3X continues... |
RESOURCES AVAILABLE FOR THE DEVELOPMENT OF
THE HFV-3X
SUPERSONIC/HYPERSONIC FLIGHT VEHICLE CONCEPT |
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SUBSONIC WIND TUNNEL
The
AeroRocket subsonic wind tunnel
is a suction system powered by a two speed 1/3 horsepower fan.
The test section is 7 inches wide x 10 inches high x 16 inches long. A research quality pitot
tube measures the difference between static and dynamic
pressure in the test section. The
resulting differential determines flow velocity using an analog velocity
meter. Small models that represent large designs are
routinely tested in the AeroRocket wind tunnel. |
SUPERSONIC SHOCK TUBE WIND TUNNEL
The AeroRocket shock tube (supersonic) wind tunnel performs
drag and lift measurements from Mach 1 to Mach 5.
The shock tube is 21 feet long or 26 feet long depending on specific Mach number
requirements. This system is operational for supersonic wind tunnel testing. Also, AeroRocket's unique expertise in the
fabrication of miniature supersonic wind tunnel models allows testing realistic shapes
for accurate flow field and CD measurements for a wide variety of R&D
applications, including the HFV-3X. |
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The HFV-3X shock tube
wind tunnel model mounted on a 1/4 inch diameter probe that
tapers to a 1.5 millimeter diameter sting. The miniature
wind tunnel model is 37
millimeters long and fabricated from a solid piece of clear
Plexiglas then painted black. |

The HFV-3X wind tunnel
model mounted on an instrumented probe designed to measure
maximum applied drag force (FX) for CD determination. |
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