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There is a renewed interest in UAVs armed with boost phase intercept missiles. David fulghum's post on ARES
http://www.aviationweek.com/aw/blogs/defense/index.jsp?plckController=Blog&plckScript=blogScript&plckElementId=blogDest&plckBlogPage=BlogViewPost&plckPostId=Blog:27ec4a53-dcc8-42d0-bd3a-01329aef79a7Post:da4f84ad-3383-42ea-9df8-0e09f25274ce
mentions two programs: Raptor Talon, which is fairly well known, and the Israeli IBIS HA-10.
This is all I could find on the subject, from Jane's website:
anyone's got pictures or more info?
http://www.aviationweek.com/aw/blogs/defense/index.jsp?plckController=Blog&plckScript=blogScript&plckElementId=blogDest&plckBlogPage=BlogViewPost&plckPostId=Blog:27ec4a53-dcc8-42d0-bd3a-01329aef79a7Post:da4f84ad-3383-42ea-9df8-0e09f25274ce
mentions two programs: Raptor Talon, which is fairly well known, and the Israeli IBIS HA-10.
This is all I could find on the subject, from Jane's website:
In 1993, Israel put forward a proposal to modify either Python 3 or Python 4 air-to-air missiles, enabling them to have a longer range to intercept tactical ballistic missiles in their boost or ascent phases. The modified missiles would have boost motor assemblies added and could be launched from aircraft or UAVs. This programme was called the Israeli Boost Intercept System (IBIS), and the missile was called the Missile Optimised Anti-Ballistic (MOAB). Reports in 1996 indicated a linkage between the IBIS programme and the US Boost Phase Intercept studies conducted by BMDO. The UAV design was completed by IAI and was believed to have the designator HA-10. The UAV would have cruised at between 7 and 15 km altitude, and would carry an IRST, laser range-finder, datalinks and two to four missiles. HA-10 was designed with low IR and radar signatures, and was planned to loiter for up to 24 hours on station with a payload of 1,000 kg. Rafael have described MOAB as a missile modified from the Python 4, by adding a boost motor assembly, giving the missile a velocity of 1.5 to 2.0 km/s and a range of 80 to 100 km. The missile would use a modified terminal IR seeker, with a laser range-finder sharing the optical path for fuze initiation. It is believed that the missile would have a length of 4.0 m, a body diameter of 0.16 m and a launch weight of 150 kg.
anyone's got pictures or more info?