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flateric said:Personally I think that this is graduate manga that obviously became Boeing paper to send someone to that boring RAS conference
compton_effect said:The most interesting bit for me is the launch flight crew - "No flight crew". That baby is flying unmanned.
Lets face it, that thing looks like something the Iranians would have thought up.
CFE said:With the added drag of the rocket, would it be possible for the F-15 to break the sound barrier in the mated configuration? I suspect that the delta-V contribution of the F-15 would be very small (certainly less than Mach 2.) If that's the case, why even bother with this concept?
In 2006, Boeing proposed a similar concept for missile launch, this time using an unmanned variant of the F-15E Strike Eagle with the launch vehicle mounted dorsally instead of ventrally. Boeing designated this variant as the F-15 Global Strike Eagle (GSE). The concept proposed the F-15 GSE as a low-cost demonstration of global strike capability utilizing a variety of munitions including the little-known Common Aero Vehicle (CAV). Defined as a maneuverable, hypersonic reentry vehicle that has the capability of dispensing a variety of payloads inside the atmosphere, the CAV concept eventually merged with the Air Force/DARPA Falcon project. Providing a Low Earth Orbit (LEO) launch capability for micro satellites, or microsats, was another mission possibility for the F-15 GSE and, with future upgrades, delivering heavier ballistic and orbital payloads.
With the added drag of the rocket, would it be possible for the F-15 to break the sound barrier in the mated configuration? I suspect that the delta-V contribution of the F-15 would be very small (certainly less than Mach 2.) If that's the case, why even bother with this concept?
Same reason that the Pegasus booster launches from the B-52, or the various Scaled Composites weirdness: to get above the thickest part of the atmosphere.With the added drag of the rocket, would it be possible for the F-15 to break the sound barrier in the mated configuration? I suspect that the delta-V contribution of the F-15 would be very small (certainly less than Mach 2.) If that's the case, why even bother with this concept?