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Peter Duniho wrote:
Robert Briggs wrote: Peter, your grasp of the physics of the matter seems to be substantially better than Don's (not that that is difficult), but I don't buy the bit about "the scramjet [being] the *entire* source of the speed". Todd's interpretation of my statement was exactly correct. This particular scramjet had limited fuel available, and all scramjets have the limitation that they only operate in supersonic flight. These limitations forced the use of a bomber and support rocket. But the thrust generated *exceeded* that provided by the rocket, which is why the scramjet was able to accelerate after being released from the rocket. Right. The flight is a *proof-of-concept* for something which would require at least one non-scramjet engine type to make a self-contained system. Yes, it has always been understood that a scramjet by itself is not very useful, since it can't be used from a standing start. Agreed. I simply think that your wording about "the scramjet [being] the *entire* source of the speed", rather than its being "sufficiently powerful to complete the acceleration to Mach 10" (or something to that effect) is a tad loose. |
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"Robert Briggs" wrote in message
... [...] I simply think that your wording about "the scramjet [being] the *entire* source of the speed", rather than its being "sufficiently powerful to complete the acceleration to Mach 10" (or something to that effect) is a tad loose. It is the entire source of the speed. Had the scramjet not been operating when it disconnected from the rocket, it would have quickly slowed to subsonic speed and of course would eventually have come to a complete stop. The speed of the rocket simply ensured proper operation of the scramjet engine...in the end, it's contribution to the final speed of the scramjet vehicle is irrelevant. An engine sufficiently powerful to accelerate the test vehicle from Mach 9 to Mach 10 is sufficiently powerful to accelerate the test vehicle from 0 mph to Mach 10. There's nothing loose about that statement at all, and it's perfectly correct. The rocket used to launch the scramjet has nothing to do with how powerful the scramjet is, or its final speed. Only the scramjet itself does. Pete |
#3
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Peter Duniho wrote:
Robert Briggs wrote: I simply think that your wording about "the scramjet [being] the *entire* source of the speed", rather than its being "sufficiently powerful to complete the acceleration to Mach 10" (or something to that effect) is a tad loose. It is the entire source of the speed. I'm not convinced, but we seem to be disagreeing about semantics, rather than about aeronautics. An engine sufficiently powerful to accelerate the test vehicle from Mach 9 to Mach 10 is sufficiently powerful to accelerate the test vehicle from 0 mph to Mach 10. Sufficiently powerful to accelerate the test vehicle from 0 mph to Mach 10, yes; actually capable of doing it, no because of the nature of the beast. The rocket used to launch the scramjet has nothing to do with how powerful the scramjet is, or its final speed. Only the scramjet itself does. The scramjet (with the aerodynamics and structural integrity of the test vehicle) sets the *possible* final speed, but the bomber and the rocket make an essential contribution to getting there. |
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