serbor, 17.02.2004 16:15:20 :
У меня вопрос реальных характеристик Барака.
Ответьте, кто может.
О реальных характеристиках вряд ли кто скажет, т.к. нет их. Вот реальные характеристики Патриота есть, но их не скажут по причинам секретности.
Вот что пишет Джейн о Бараке (янв. 2003):
TITLE : Barak/ADAMS/'Relampago'/Defender
TEXT :
Type
Short-range, ground- and ship-based, solid propellant, theatre defence
missile.
Development
Studies for the development of a small and lightweight vertically launched
surface-to-air missile started in Israel in 1979. The Barak 1 ship-based
system, designed and developed jointly by IAI and Rafael, was first seen
at the 1983 Paris Air Show. Vertical launch trials started in 1984, and
the first trials engagement of a simulated sea-skimming missile was
successfully completed in 1986. Sea trials began in 1989. Barak is being
fitted to 'Hetz' class fast attack craft (Saar 4.5) with 16 or 32 cell
vertical launchers, and to 'Eilat' class corvettes (Saar 5) with two 32
cell vertical launchers for the Israeli Navy. The missile is also being
fitted to 'Prat' (ex-UK 'County') class destroyers with two octuple
launchers for the Chilean Navy, and Singapore is adding two octuple Barak
launchers to its 'Victory' class corvettes. A scaled-up version of the
Barak missiles, designated AB-10 was proposed as a short range ATBM in
1987, but this programme was terminated in 1989. A ground-based version,
known as ADAMS (Air Defence Anti-Missile System), was reported to be in
development in 1991, with up to 12 vertically launched missiles carried on
an 8 x 8 wheeled vehicle together with the tracking radar and an
electro-optical sensor for use in heavy ECM environments. Hughes Missile
Systems (now Raytheon Missile Systems) proposed the ADAMS missile combined
with the Phalanx gun as the HVSD/ADAMS for the US DoD high value site
defence system. In 1994, a ground-based Barak system was again offered for
export, this time called 'Relampago' and mounted on an 8 x 8 wheeled
vehicle with 12 missiles in VL canisters and engagement radar with EO
tracker. The 'Relampago' system was reported to be capable against
aircraft, helicopters, missiles and UAVs.
An export order to Venezuela, announced in 1998, is believed to
incorporate the 'Relampago' system with Signaal Flycatcher Mk2 weapon
control systems, Lirod Mk2 radars and Mirador EO sighting systems. In 2001
a ground-based version called Defender, was proposed for use by NATO
countries, with the introduction of NATO standards through a joint teaming
arrangement with Thales.
In May 2002 proposals were made by IAI for a Barak Mk 2 missile system,
to meet the Israeli Navy requirements for a Next-Generation Defence
Missile (NGDM) for the upgraded Eilat class (Saar 5 plus) corvettes.
Description
The Barak 1 missile has four folding clipped-tip delta-wings and four
folding moving clipped-tip control fins at the rear. The missile is 2.17 m
long, has a body diameter of 0.17 m, an unfolded wing span of 0.68 m, and
weighs 98 kg. In addition to the control fins, there are thrust deflectors
in the boost motor exhaust nozzle to assist in controlling the missile
after its vertical launch. The boost motor section is ejected on
completion of the initial boost phase. Guidance is by radar-controlled
Command to Line Of Sight (CLOS), using an Elta STR M2221 coherent
pulse-Doppler radar, or using an electro-optic tracker in severe ECM
conditions. The STR engagement radar operates in the 8 to 40 GHz
(X/Ka-bands), has an elevation coverage of +85 to -25є and a range of
about 20 km. The Barak missile warhead weighs 22 kg, and is a
fragmentation type with an active laser fuzing system that is supported by
an altimeter to allow the interception of very low level targets. The
missile has a range of 12 km against aircraft targets, and probably about
5 km against sea-skimming anti-ship missiles. A minimum range of 500 m is
reported. The lightweight system including radar, fire-control system and
eight missiles in launch canisters weighs a total of 3,000 kg. The
fire-control radar can command two separate missiles towards each target
and it is reported that the Barak system can be fully automatic under the
control of the threat evaluation system.
Operational status
Development started in 1983 but the Barak missile programme was funded at
low level. Sea trials began in 1989 and the first Barak firing at sea was
successfully carried out in 1991, with a successful interception of a
Gabriel anti-ship missile in 1993. Barak 1 is reported to have entered
service with the Israeli Navy in 1994. Missiles have been fitted to the
'Hetz' class Fast Attack Crafts (FACs), and to 'Eilat' class corvettes
(Saar 5). Barak has been exported to Chile, to be fitted to four Prat
class, former UK 'County' class destroyers, and to Singapore for its
'Victory' class corvettes. Singapore fired a small number of missiles
during exercises in July 1999. Trials have also been reported from South
Africa, with several Barak missile firings being made there in 1991.
Venezuela ordered three mobile land-based systems in 1998, to be
integrated with Flycatcher Mk 2 weapon systems for airfield defence. India
ordered Barak missiles in November 2000 and these have been fitted to the
aircraft carrier INS Viraat, with two octuple VLS launch cells. India may
fit the missiles into Rajput class (Kashin II type 61ME) destroyers and
modified Godavari (type 16A) frigates.
SPECIFICATIONS :
Specifications
Length: 2.17 m
Body diameter: 0.17 m
Launch weight: 98 kg
Warhead: 22 kg HE fragmentation
Guidance: CLOS
Propulsion: Solid propellant
Range: 12 km
Associated radars
Engagement radar: Elta STR
Frequency: 8-40 GHz (X/Ka-band)
Peak power: n/k
Range: 20 km