Maddog (Все сообщения пользователя)

The SM-3 was a derivative of the Standard SM-2ER Block IV using the LEAP (Lightweight Exo-Atmospheric Projectile) homing vehicle to give AEGIS naval vessels theater anti-ballistic missile capability. The two rocket stages of the SM-2ER Block IV were supplemented by a third stage, the Alliant Techsystems Advanced Solid Axial Stage (ASAS). A [U][B]GPS-Aided Inertial Navigation System was used to guide the missile to near the predicted impact point, with the LEAP making the final hit-to-kill intercept.[/B][/U] AEGIS launching ships required updates to computer hardware and software in order to operate the missile.
Т.е. с подавлением GPS эта хрень работать не будет.
The LEAP and its Forward-Looking Infrared sensor were first tested in four Terrier/LEAP launches between 1992 to 1995. However both intercepts attempted in the series were failures. The first launch of a complete SM-3 missile came in September 1999. In January 2002 the first successful intercept of an Aries ballistic missile target was achieved. Testing thereafter proved the capability of the missile against more difficult targets and scenarios. In 2008 the system was modified in a matter of weeks to successfully shoot down an errant American satellite.

Failures: 1. First Fail Date: 2000-07-01. Last Fail Date: 2000-07-01. Maximum range: 500 km (310 mi). Standard warhead: LEAP. Boost Propulsion: Solid rocket. Cruise engine: MK 104. Maximum speed: 9,600 kph (5,900 mph). Initial Operational Capability: 2006.

AKA: SM-3;RIM-161A;Standard 3 ER.
Status: Active.
Gross mass: 1,500 kg (3,300 lb).
Height: 6.55 m (21.48 ft).
Diameter: 0.53 m (1.73 ft).
Span: 1.57 m (5.15 ft).
Apogee: 160 km (90 mi).
First date: 1999-09-24 .
Last date: 2009-07-31 .
Number: 22 .
Для атмосферного перехвата на таких скоростях для ИК ГСН нужно сапфировое окно - не впишутся в US$ 1 000 000.
И чем они собираются охдаждать ГСН - жидким азотом?