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#1
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Widely reported where? This is going to sound like a copout but I read a LOT. It could have been any number of places but I know I've seen it numerous times and I RARELY rely on company propaganda for information. Usually company sites are good for photos or videos (except for the exceptionally lame Northrop Grumman site). If you look at the Raytheon site http://www.raytheon.com/products/aim9_x/ you'll see that the canard configuration is similar to the AIM-9M. The canards are much smaller and fixed. Some improvement in range is possible. Much higher is questionable. ASRAAM and Python have much larger motors for the same generation seeker technology (same seeker in ASRAAMs case) indicating that designers not tied to a large stock of existing ordnance feel that more impulse can be usefully employed exploiting the seeker's performance. IIRC all the rest of the entries for which the -9x as-is was selected had bigger motors too. |
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#2
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"Scott Ferrin" wrote Some improvement in range is possible. Much higher is questionable. ASRAAM and Python have much larger motors for the same generation seeker technology (same seeker in ASRAAMs case) indicating that designers not tied to a large stock of existing ordnance feel that more impulse can be usefully employed exploiting the seeker's performance. IIRC all the rest of the entries for which the -9x as-is was selected had bigger motors too. Yep, they did. The USAF perhaps feels less need for a long range IR missile since AIM-120 fills that range bin. |
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#3
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Paul Austin wrote:
"Scott Ferrin" wrote Some improvement in range is possible. Much higher is questionable. ASRAAM and Python have much larger motors for the same generation seeker technology (same seeker in ASRAAMs case) indicating that designers not tied to a large stock of existing ordnance feel that more impulse can be usefully employed exploiting the seeker's performance. IIRC all the rest of the entries for which the -9x as-is was selected had bigger motors too. Yep, they did. The USAF perhaps feels less need for a long range IR missile since AIM-120 fills that range bin. Exactly right. That, and they had a lot of AIM-9s (at least half of the 24,000 in stock) available to convert. FWIW, here's some data from the Air International article "Battle of the Missiles" by John Fricker in the Feb. 1997 issue: "Two Sidewinder-derived reduced airframe drag configurations were proposed by the Pentagon in April 1993, as AIM-9X options. From the USAF came the wingless Box Office concept, using very small (28cm/11 in span) all-moving tail-mounted fin controls, with no foreplanes, plus digital autopilot stabilisation, while the Naval Weapons Center's relaxed stability Boa project employed a clipped canard and fin configuration (40.64cm/16 in. span each), with a similar autopilot." "In broad terms, Box Office was expected to halve the drag of the current AIM-9M8/9 and double its 8km (4.3nm) range. A speed increase of up to Mach 1.3 over the original Mach 2.5 was also sought, with doubled g-limits. Boa has higher drag and hence a reduced range and maximum speed, but it has less speed loss in turns. . . ." "AIM-9X seeker performance targets included increasing clear sky target acquisition range to 13-16km (7 - 8 3/4 nm) and 6.6km (3 1/2 nm) in ground clutter. . . ." He then goes on to give descriptions of the Iris-T, ASRAAM, P4 and Magic 2 and their variants on offer, and says why each was rejected. The design eventually selected was a Hughes version called Box Office 2 Plus, although it seems to have the clipped canard/fins Fricker attributes to Boa. Guy |
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