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What is the maximum range of air defense missiles?
LEAP used forward-looking infrared sensor (FLIR) to locate the target, and carried out four launch tests on beagle missile from 1992 to 1995. The improved Beagle and Standard 2 missiles were used in the experiment, and two interception launches were attempted, but both failed. The first test of RIM- 16 1A SM-3 was carried out in September 1999, and the third test in 200 1 year1October successfully carried out the missile flight and separated the kinetic energy warhead. June 5438+October 2002 10, RIM- 16 1A conducted the first successful full-range experiment and hit the Aries ballistic missile.
The development of the Standard -3 interceptor missile shows that the early launch test also failed. The fixed steering and attitude control system (SDACS) used in the interceptor warhead failed in the launch test codenamed "FM5" on June 18, 2003. This test is the first time to test SDACS in a real simulation scenario. The launch test of "FM-6" successfully intercepted the target in 2003, but the SM-3 plan still showed obvious delay. The "FM-7" experiment was postponed several times and finally carried out on February 24, 2005. In this experiment, the standard RIM- 16 1A missile is used.
In mid-2006, the experiment of SM-3 was carried out as scheduled. On June 22nd, 2006, the latest BlockIA missile (No.RIM- 16 1B) was used and successfully intercepted. RIM- 16 1B is characterized by upgrading the missile engine and guidance control software to enhance the overall performance, including changes in production and maintenance design.
Future planned RIM- 16 1 missiles include RIM- 16 1C Block IB, which uses a two-color seeker and a new steering and attitude control system. The Block II series will also add other improvement measures, including the second and third stage rocket engines, which will increase the diameter of the missile to improve the maneuverability of the missile.
Other data of RIM- 16 1A:
The length of the bomb (including booster) is 6.55 meters.
Span1.57m.
The diameter of the bullet is 0.34 meters.
Unknown weight
The launch speed of the standard -3 interceptor missile is 9600 km/h.
Shooting height >160km (100 miles)
Propulsion device: United Technologies MK 72 solid rocket
Main engine: MK 104 dual-thrust solid rocket of Atlantic Research Corporation.
Third stage engine: Alliant Techsystem MK 136 solid rocket.
Warhead: collision kinetic energy warhead
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