Development of the HFV-3X
Hypersonic Flight Vehicle
  HFV-3X Wind Tunnel Model
HFV-3X Hypersonic Aircraft Wind Tunnel Model
HFV-3X Wire Frame
HFV-3X Hypersonic Aircraft AeroWindTunnel Wire Frame Design
 

HTV-3X (Blackswift) DesignIntroducing 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
HTV-3X in the subsonic wind tunnel AeroRocket shock tube
Shock-Tube Diaphragm or Rupture-Disk

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.

HFV-3X shock tube model
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.

Shock tube test section with model
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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