*Range estimates assume equal 10,000 ft altitudes, Mach 1 speed, head-on aspect parameters.*Ĭapabilities: ECCM, Home-on-jam, MPRF (Pitbull) for all-aspect targets and HPRF (Husky) for high-closure rate targets. Motor: WPU-6/B - Hercules solid rocket motor Radar proximity range: PROPULSION/CONTROL Warhead: WDU-33/B - 22.7kg annular blast fragmentation (198x projectiles) įuze: FZU-49/B - Active radar proximity and impact Loft max altitude: 14km (65km target distance) Guidance type: Command inertial, mid-course autonomous inertial, terminal active radarÄ«attery: Lithium-aluminum - 80 sec lifespan Notes: Pulse compression, programmable waveforms, traveling-wave-tube amplifier PRF: MPRF (Pitbull) for all-aspect targets and HPRF (Husky) for high-closure rate targets Seeker: Hughes I/J-band monopulse active radar (8 to 10 GHz) *Range estimates assume equal 10,000 ft altitude, Mach 1 speed, head-on aspect parameters.*Ärag coefficient (cD, 0° ): 0.016 ( ![]() Due to this problem, Canada withdrew their order, and Finland placed theirs on hold." "The AMRAAMâs most significant fault is that it is prone to engine malfunction in cold weather. The AMRAAM has enjoyed a high success rate in operational service while also being fairly reliable. Followed by several Serbian aircraft shoot-downs by US and allied F-16 and F-15s over Kosovo in 1999. Shortly after, on January 17, 1993, another US Air Force F-16C shot down an Iraqi MiG-29 Fulrum. Full-rate production of the missile was approved in April 1992." The missile flew in Desert Storm, but did not achieve its first aerial victory until Decemwhen a USAF F-16D shot down an Iraqi MiG-25 over Southern Iraq: ( ). The F-16 followed in January 1992, and the Navy in October 1993. "In September 1991, IOC (Initial Operational Capability) was achieved for the AMRAAM on USAF F-15 aircraft. Originally designated the AIM-120C-8, for P3I Phase 4, this was a major improvement that included modifications such as a 50% increase in range, and two-way datalink. This would culminate in 2008 as the AIM-120D would begin testing. In 1991 the Pre-Planned Product Improvement (P3I) program was initiated and would incrementally upgrade the new AIM-120C model for decades to ccome, with variants C-3 to C-7. Which was a relatively minor guidance and electronics upgrade over the 120A model. Several upgrades would llater improve on the AIM-120 series, starting with the AIM-120B in 1198. Initially the AIM-120 was developed as a complement to the European development of a short-range IR missile (ASRAAM). ![]() ![]() Objectives for the program included: higher speed, further range, lower weight, improved maneuverability, ECCM capability, improved maintainability and reliability. The AMRAAM (Advanced Medium Range Air to Air Missile) development program began in 1975 as a joint US Air Force and Navy study that contracted Hughes and Raytheon (who later merged into a single company) to develop an active radar replacement for the AIM-7 Sparrow missile series. *Detailed specifications on the AIM-120 missile series, especially the more recent variants, are highly classified as this missile is used regularly in many countries' air forces.*
0 Comments
Leave a Reply. |
Details
AuthorWrite something about yourself. No need to be fancy, just an overview. ArchivesCategories |