As the shiny drum rolls across the stage. lol
Anyway... comparisons here to what may have completely solved the Aurora case once and for all...
X-30 side:
found on the FAS Site
Prior analyses of scramjet propulsion systems had concluded that they would only be able to achieve speeds of about Mach 8. At this speed, the thrust
emerging from the rear of the plane would be balanced by the heat generated by atmospheric drag and the high temperature of the air as it entered the
front of the engine. Thus limited to a maximum speed that was only one-third the orbital velocity of Mach 25, a scramjet-propelled vehicle would need
rocket motors to achieve the remaining speed needed to reach orbit. Analyses concluded that such a vehicle would be heavier and more complicated that
a conventional rocket.
However, the Copper Canyon project discovered that higher speeds could be achieved through the imaginative use of active thermal management. By
circulating, and thus heating, the scramjet's hydrogen propellant through the skin of the vehicle prior to injection into the engine, energy
generated through atmospheric drag was added to the thrust of the scramjet, enabling it to accelerate beyond the Mach 8 thermal barrier. Initially,
there was optimism that this active thermal management approach would permit speeds of up to Mach 25 using air- breathing engines alone, eliminating
the need for rocket propellants to achieve orbit
Now the specifications I've managed to scrape up are as follows:
Speed: Roughly Mach 23 or 17,549 MPH (sorry don't do km/h)
Altitude: out of atmosphere 200,000+ feet
Engine type: Scram Jet or Pulse Detonation Wave Engines
Main Mission: Reconnasaince
Armament: None
Aurora XST side:
Adding a link first for an error made in a previous post:
www.fas.org...
specifications found on BlackVault
Speed: Maximum operational speeds are reported to be in the range of Mach 5-8.
Ceiling: May have an operational altitude of 150,000 feet (28.4 miles) or higher.
Engine type: Scram jet or Pulse Detonation Wave Engines
Armament: Possibly Phoenix Missiles
Main Mission: Reconnasaince
All together specifications
Speed: Roughly Mach 15 or 11,445 MPH
Ceiling: 185,000+ feet
Engine type: Scram jet or Pulse Detonation Wave Engines
Armament: Possibly Phoenix Missiles
Main Mission: Reconnasaince
Average the two:
Speed: 14,497 MPH or Mach 19
Ceiling: Out of Atmosphere
Engines: Scram/Ramjets or PDWE's
Armament: Probably Phoenix Missiles
Most Likely to be a recon/interceptor.
Another candidate for current sonicbooms and being mistaken for Aurora (X-30) which has now in my eyes been de-classed, is the X-43A Hyper-X, what's
the problem with the X-43? Why isn't it thought to be Aurora? Take a look at the links and specs below you'll know why.
The X-30 was not supposed to be fired as a rocket. Nor was it a rocket.
www.air-and-space.com...
www.fas.org...
The multi-year NASA/industry Hyper-X program seeks to demonstrate airframe-integrated, "air-breathing" engine technologies that promise to
increase payload capacity for future vehicles, including hypersonic aircraft (faster than Mach 5) and reusable space launchers. The X-43 will be the
first free-flying demonstration of an airframe-integrated, air-breathing engine and will extend the flight range to Mach 10.
Close but, not close enough.
I think it's pretty much safe to say that the Aurora is in fact the X-30.