X-51 presentation.http://sfte2013.com/files/78961102.pdf
Quote from: Star One on 07/30/2014 10:10 amX-51 presentation.http://sfte2013.com/files/78961102.pdfInteresting presentation on the nuts and bolts of running such a test and, incidentally the sort of issues that launching a wing mounted LV would probably face. I guess the bottom line is for successful results, check and test everything and have a backup plan for plausible failures involving any part of the team or their equipment.
One thing that I found curious from a quick glance through it, is that it talks of carrying any future weapon developed from it internally on a B-2 or externally on the F-35. But why not mention the LRS-B which I would have thought the main platform for it, it's not like the existence of the program is a secret?
Quote from: Star One on 07/30/2014 03:05 pmOne thing that I found curious from a quick glance through it, is that it talks of carrying any future weapon developed from it internally on a B-2 or externally on the F-35. But why not mention the LRS-B which I would have thought the main platform for it, it's not like the existence of the program is a secret?This is at present only a potential weapson system and I think it's fair to say so is the LRS-B, the B-2 and F35 OTOH are live deployed platforms.
Quote from: john smith 19 on 07/31/2014 08:35 pmQuote from: Star One on 07/30/2014 03:05 pmOne thing that I found curious from a quick glance through it, is that it talks of carrying any future weapon developed from it internally on a B-2 or externally on the F-35. But why not mention the LRS-B which I would have thought the main platform for it, it's not like the existence of the program is a secret?This is at present only a potential weapson system and I think it's fair to say so is the LRS-B, the B-2 and F35 OTOH are live deployed platforms. My curiousity was tickled by the fact they didn't mention external carry on the F-22... For the last decade EVERY "future-weapons-system" in the pipe has been shown on every platform specifically including the F-22/35. I had access to books that showed the mounting points for everything up to and including the SAL (Surface Attack Laser pods that never got tested) and hypersonic attack missiles. Not mentioning the F-22 as a carrier platform is very interesting to me (And before anyone asks, no about 2/3rds of the systems depicted are/were never fully developed but the easyist thing to figure out is where to put them on an airframe if you have a general clue to what they might be shaped like and/or weigh )Randy
Does it make any sense to carry it on an F-22?
It wouldn't be terribly good as a replacement short range missile where a rocket motor is better for hitting other aircraft.
You'd want one for medium and long range strikes, and that means you're going after fixed or slow targets that can potentially defend themselves, so the developers will want a correspondingly large warhead. So quickly, it becomes a weapon for tactical or strategic bomber mounting and not fighter mounting.
Mentioning that such a weapons system "can" be carried externally (really there's no hope of carrying something of the assumed size of a hypersonic strike missile "internally" on a fighter airframe in the first place so why that's mentioned that way is another question) on a "fighter" makes sense but suggesting that such an airframe would be the F-35 is going to make a lot of people sit up and take notice in the wrong way any way "I" look at it. And I can't shake the feeling that's exactly what and why it was done...
I don't think it'll be an F-35 mounted weapon at all (nor an F-22 weapon). More like a B-2 and B-3 mounted weapon.
Oh and since we're going in that direction I'll point out again that the ASLAM was a SUBSONIC combustion ramjet engine and IT did Mach-5.5 by ACCIDENT with a non-optimized inlet and exhaust so... Tell me again why we "need" a SCramjet engine in the first place?Let me drop a few other links while I'm at it:The French tested a Mach-5 (subsonic combustion) Missile in 1966:https://archive.org/details/nasa_techdoc_19670008070