X-33

ASTRA Program

ASTRA Home page

Waverider

X-Craft

 

 

 

 

 

 

 

 

 

 

If you haven't already done so

Please Sign ASTRA's Guestbook 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Should you wish to contact the society or require general information please contact ASTRA using the following Email address:

info@astra.org.uk

 

 

 

 

 

 

 

 

 

Should you encounter any problems with this Web Page please email:

portwin@easynet.co.uk

 

X-33 Ground Technology

The X-33 test vehicle would takeoff in a vertical position and use conventional runways to land horizontally. The entire spaceplane (with all fuel tanks and engines) would takeoff and land as a single unit.

 

During the landing sequence, the spaceplane would glide to the landing site in an unpowered manner. Flight tests would involve speeds of up to Mach 15 and altitudes up to approximately 75,800 meters (250,000 feet). None of the X-33 tests flights would achieve Earth orbit. Ground operations and servicing (e.g., checkout, refuelling, etc.) would be conducted with ``aircraft like'' procedures and systems.

After each test flight, the X-33 would be ferried back to the takeoff site by a Boeing 747 aircraft in a manner similar to that used for the transport of Space Shuttle orbiters.

 

RLV Potential Operational Attributes

The RLV will be designed as a means of transport only. It is not intended to be used as a science platform like the Space Station and Space Shuttle.

Crew members will probably be transported to and from the Space Station in a containerized passenger module as shown in this image.

The RLV will be designed from the beginning for streamlined operations. A simplified operations plan employing a minimal ground support staff will be established and the hardware designed to accommodate the plan, rather than vice-versa.

The RLV will feature innovations in materials processing, assembly, and maintenance and support techniques designed to reduce the costs and manpower associated with constructing and operating a space transportation system.

 

New technologies being developed include the light-weight composite and aluminum-lithium fuel tanks, a full-scale Linear Aerospike Engine, modular primary vehicle structures, and a metallic thermal protection system.

 

The RLV fleet will be certified by a comprehensive testing program before operations begin. All operational flights will be flown well within the established limits of the vehicle.

The X-33 is an integrated lifting body / aerospike engine configuration. The X-33 is a vertical takeoff / unpowered horizontal landing single stage spaceplane. Lift is generated during reentry and landing via its "wedge" shaped platform. Separate wings are not required. Do not use these scale for engineering purposes.

 

The X-33 will launch from Edwards Air Force Base in California and land at one of three test sites. The vehicle is processed horizontally within a translating shelter, rotated to the vertical position, and then launched. Upon landing the X-33 is returned to the launch site via the NASA-747 Shuttle Carrier Aircraft.

Click here to return to top of this page

ASTRA A to Z

ASTRA Program | ASTRA Home Page | Waverider Home Page | X-Craft

 

XB-70 | X-15 | X-20 | X-33 | X-34 | X-38 | Future-X

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