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PostSubyek: Calon Bomber Pengebug yg sgt diminati RI jika jd HIGHPROFILE postur pertahanan   Thu Sep 16, 2010 11:38 am

The Tupolev Tu-22M (Туполев Ту-22М) (NATO reporting name: Backfire) is a supersonic, swing-wing, long-range strategic and maritime strike bomber developed by the Soviet Union. Significant numbers remain in service with the Russian Air Force.


The Tupolev Tu-22 had not proved particularly successful, in some respects being inferior to the earlier Tu-16. Its range and take-off performance, in particular, were definite weak points. Even as the Tu-22 was entering service, OKB Tupolev began work on an improved successor.

As with the contemporary MiG-23 and Su-17 projects, the advantages of variable-geometry wings seemed attractive, allowing a combination of short take-off performance, efficient cruising, and good high-speed, low-level ride. The result was a new swing-wing aircraft called Samolyot 145, derived from the Tu-22, with some features borrowed from the abortive Tu-98. The Tu-22M was based on the Tu-22's weapon system and used its Kh-22 missile. The Tu-22M designation was used to help get approval for the bomber within the Soviet system.[1]

The first prototype, Tu-22M0, first flew on 30 August 1969. The resultant aircraft was first seen by NATO around that time. For several years it was believed in the West that its service designation was Tu-26. During the SALT negotiations of the 1980s the Soviets insisted it was the Tu-22M. At the time, Western authorities suspected that the misleading designation was intended to suggest that it was simply a derivative of the Tu-22 rather than the more advanced and capable weapon it actually was.

Operational history

During the Cold War, the Tu-22M was operated by the VVS (Soviet Air Force) in a strategic bombing role, and by the AVMF (Aviatsiya Voyenno-Morskogo Flota, Soviet Naval Aviation) in a long-range maritime anti-shipping role.[2]
Tu-22M3 in 2004 at Monino near Moscow

The Tu-22M saw its first combat use in Afghanistan from 1987 to 1989. A Tu-22m during landing and taxing can be seen here:[1]. Its usage was similar to the United States Air Force deployment of B-52 Stratofortress bombers in Vietnam War, dropping large tonnages of conventional ordnance. The Russian Federation used the Tu-22M3 in combat in Chechnya in 1995, carrying out strikes near Grozny.[2]

At the time of the break-up of the USSR, some 370 remained in CIS service. Production ended in 1993. The current strength was about 162 aircraft in 2008,[3] with an additional 93 in reserve.

Russian military officially acknowledged the loss of a Tu-22MR bomber to Georgian air defenses early in the 2008 South Ossetia war.[4][5] One of its crew members was captured (Major Vyacheslav Malkov), two others were killed and crew commander is missing in action as of August 2009.


The Soviet Union did not export the Tu-22M, but the break-up of the USSR left some aircraft in the possession of former Soviet republics. Belarus has 52 (the serviceability of which is unclear). Ukraine had an additional 29, but since the Ukrainian government's renunciation of nuclear weapons, those aircraft have been destroyed, the last in 2004.

Tupolev has sought export customers for the Tu-22M since 1992, with possible customers including Iran, India and the People's Republic of China, but no sales have apparently materialized. Four were leased to India in 2001 for maritime reconnaissance and strike purposes


Only nine of the earliest Tu-22M0 pre-production aircraft were produced, followed by nine more Tu-22M1 pilot-production craft in 1971 and 1972. Its NATO reporting name was Backfire-A.

The first major production version, entering production in 1972, was the Tu-22M2 (NATO: Backfire-B), with longer wings and an extensively redesigned, area ruled fuselage (raising the crew complement to four), twin NK-22 engines with F-4 Phantom II-style intakes, and new undercarriage carrying the landing gear in the wing glove rather than in large pods. These were most commonly armed with long-range cruise missiles/anti-ship missiles, typically one or two Raduga Kh-22 anti-shipping missiles. Some Tu-22M2s were later reequipped with more powerful NK-23 engines and redesignated Tu-22M2Ye. In service, the Tu-22M2 was known to its crews as Dvoika ('Deuce').

The later Tu-22M3 (NATO: Backfire C), which first flew in 1976 and entered service in 1983, had new NK-25 engines with substantially more power, wedge-shaped intakes similar to the MiG-25, wings with greater maximum sweep, and a recontoured nose housing a new Leninets PN-AD radar and NK-45 nav/attack system, which provides much-improved low-altitude flight (although not true nap-of-the-earth flying). It had a revised tail turret with a single cannon, and provision for an internal rotary launcher for the Raduga Kh-15 missile, similar to the American AGM-69 SRAM. It was nicknamed Troika ('Trio'), although apparently it is sometimes referred to as Tu-22 in Russian service.
Closeup of the refuelling probe of a Tu-22M1

One area of controversy surrounding the Tu-22M is its capacity for aerial refueling. As built, the Tu-22M has provision for a retractable in-flight refueling probe in the upper part of the nose. This was allegedly removed as a result of the SALT negotiations,[8] although it can be easily reinstated if needed,[2] and a pre-production Tu-22M1 (NATO: Backfire-A) with refueling probe can be seen at Riga Airport today.

A small number, perhaps 12, of Tu-22M3s were converted to Tu-22M3(R) or Tu-22MR standard, with Shompol side-looking radar and other ELINT equipment.[2] A dedicated electronic warfare variant, designated Tu-22MP, was built in 1986, but to date only two or three prototypes have apparently been built. Some surviving Tu-22s have had equipment and avionic upgrades to Tu-22ME standard (which does not have a separate NATO reporting name at this time).

Total production of all variants was 497 including pre-production aircraft

Specifications of Tu-22M3
Orthographic projection of the Tupolev Tu-22M
Loading Raduga Kh-15 missiles onto rotary launcher
A Raduga Kh-22 anti-ship missile under a Tu-22M3

General characteristics

* Crew: 4 (pilot, co-pilot, bombardier, defensive systems operator)
* Length: 42.4 m (139 ft)
* Wingspan:
o Spread (20° sweep): 34.28 m (112 ft 6 in)
o Swept (65° sweep): 23.30 m (76 ft 5 in))
* Height: 11.05 m (36 ft 3 in)
* Wing area:
o Spread: 183.6 m² (1,976 ft²)
o Swept: 175.8 m² (1,892 ft²)
* Empty weight: 58,000 kg (172,000 lb)
* Loaded weight: 112,000 kg (247,000 lb)
* Max takeoff weight: 126,000 kg (277,800 lb)
* Powerplant: 2× Kuznetsov NK-25 turbofans, 245 kN (50,000 lbf) each


* Maximum speed: Mach 2.05 (2,327 km/h,)
* Range: 7,000 km (4,971 mi)
* Combat radius: 2,410 km (1,500 mi)
* Service ceiling: 13,300 m (40,635 ft)
* Rate of climb: 15m/s (91ft/s)
* Wing loading: 688 kg/m² (147 lb/ft²)
* Thrust/weight: 0.40


* Guns: 1 × 23 mm GSh-23 cannon in remotely controlled tail turret
* Hardpoints: wing and fuselage pylons and internal weapons bay with a capacity of 21,000 kg (46,300 lb) of

* From up to 3 × Raduga Kh-22 missiles in weapons bay and on wing pylons or
* The Tu-22M3 can carry six missiles on a MKU-6-1 rotary launcher in its bomb bay, plus four missiles on two underwing pylons for a total of ten missiles per aircraft.or
* Various freefall bombs - 69 × FAB-250 or 8 × FAB-1500 might be typical.

The Kh-55 (AS-16 'Kent') long-range cruise missile was tested on the Tu-22M[9] but apparently not used in service.

Tupolev Tu-22M3 Backfire C Bomber - Missile Carrier

The Tupolev Tu-22M3 Backfire C is in a class of its own. In conceptual terms, it could best be considered a larger supersonic equivalent to the RAF's 1960s V-bombers, armed with a more evolved equivalent to the RAF's Avro Blue Steel Mk.1 supersonic standoff missile. The Backfire remained in production until 1993, and given low flying hours, the extant Russian fleet is largely younger in airframe hours than the US B-1B Lancer fleet.


With the recent public exposure of the PLA's Xian H-6K turbofan powered Badger cruise missile carrier it is clear that the PLA is moving ahead with its planning for a strategic bomber fleet with more reach than the legacy H-6 Badger variants, under the auspices of the "Second Island Chain Strategy". Off the shelf candidates for this fleet include upgraded surplus Russian Air Force Tu-22M3 Backfire C and Tu-95MS Bear H aircraft, and new build Tu-160 Blackjacks, as well as the indigenous and smaller H-6K. In 2005 the Chief of Air Staff of the Russian Air Force observed, in relation to the Backfire and Bear, that surplus aircraft should be exported to China.

In terms of time to deployment and acquisition cost, the Backfire is strong contender in any competitive flyoff between these types. To best appreciate the potential strategic impact of the Backfire upon this region APA will explore the capabilities and further growth potential of the aircraft in more detail.

The underpowered Tu-22M2 Backfire B was the first production model, or which over 200 were built (US DoD).

The Tupolev Tu-22M3 Backfire C

The latest variant of the Backfire is the third generation Tu-22M3 Backfire C model, which remained in production until 1993.

The earliest origins of the Backfire were in the earlier Tu-22 Blinder, a Russian analogue to the US B-58 Hustler. Inferior to the B-58, the Soviet air staff sought a significantly more capable design. After much research and internal argument during the mid 1960s, the Tu-22M designation was allocated to a largely unique design.

The first Backfire variant was the Tu-22M-0 subtype, using an F-4 Phantom like inlet arrangement, long inlet tunnels, a variable geometry wing, and B-1A-like side by side seating, unlike the tandem Tu-22 Blinder. A pair of NK-144-22 afterburning fans, common to the Tu-144 Concord-ski were employed. The embryonic Backfire inherited the single centreline Raduga Kh-22/AS-4 Kitchen [More ...] supersonic standoff missile as its primary weapon. Flight testing progressed concurrently with low rate initial production, but only 10 were built by late 1972.

Dissatisfaction with the baseline Backfire led to an extensive rework of the design, under the designation Tu-22M-1 or Backfire A. Aerodynamics were refined, 6,500 lb of weight removed, span was increased by 60 inches and the speedbrake was relocated. The Backfire A was also a disappointment, and only 9 were built by late 1972.

Yet another cycle of redesign work followed, producing the Tu-22M-2 or Backfire B designated article 45-02, the first mass production variant. It was around 3,000 lb lighter than the Backfire A, and powered by a pair of new NK-22 engines. With more thrust, the Backfire B could lift up to 24 tonnes of weapons, including a payload of three Kh-22/AS-4 Kitchen missiles. The aircraft carried a tail turret with paired NR-23 guns, a PRS-3 Argon-2 ranging radar and TV remote gunsight. The PNA-B Rubin / Down Beat attack radar was designed to provide over 300 degree coverage emulating the HP Victor installation, and was supplemented by a ventral remote TV bombsight arranged like that in the Avro Vulcan. Dal'naya Aviatsia IOC was achieved in 1974, with AV-MF naval aviation regiments receiving their Backfire Bs in 1976. By the end of production in 1983, no less than 211 examples were built.

The underpowered Backfire B was considered inadequate and design work commenced early on the improved Tu-22M3 or Backfire C designated Article 45-03, which first flew in 1977, following trials of the more powerful NK-25 engine in a Backfire B airframe. The redesign was extensive, including some use of titanium structure to further reduce empty weight, and was led by the Tupolev Bureau's Deputy Chief Designer Boris E Levanovich. The most visible change were the adoption of F-15 style ramped inlets, and revised auxiliary inlets. Less visible were changes to the wing design, permitting a 65 degree sweep, more than earlier variants. The reshaped and stretched nose incorporated a revised refuelling probe design. Further changes were made to the vertical tail, undercarriage, defensive gun package and avionics. During the mid-1990s the author discussed the Tu-22M3 with Levanovich, who was adamant that the production aircraft had a hi-hi-hi combat radius of 4,000 km (2,160 NMI) with a payload of three Kh-22M/AS-4 missiles, well in excess of then current Western estimates.

Detector aperture for the L-082 MAK-UL series infrared MAWS, here installed on a Bear H (©️ Miroslav Gyűrösi).

Emitter array for internal SPS-171/172 electronically steerable jammer, depicted in podded configuration (KNIRTI).

Terminal hard kill defensive capability in the aft sector is provided by a UKU-9A-802 tail barbette, fitted with a single GSh-23 gun, and directed by an improved PRS-4KM Kripton / Box Tail ranging radar and remote TV camera.

Avionic improvements were no less extensive. The Avtomat 3 Radar Warning Receiver was fitted, with an internal variant of the KNIRTI SPS-171/172 Sorbstiya wideband phased array jammer (refer image) and the AG-56 automated nosie generator also carried. The SPS-171/172 is claimed to provide noise and deception jamming modes, and is available podded as the L-005 for the Su-27/30. The UKU-9A-802 tail barbette was fitted with a single GSh-23 gun, supported by an improved PRS-4KM Kripton / Box Tail ranging radar and remote TV camera. Ventral and dorsal infrared L-082 MAK-UL series Missile Approach Warning System (MAWS) turrets are fitted to many aircraft.

The ventral OBP-15T remote TV bombsight is used to target dumb bombs. The fairing for this device is well placed to fit an infrared imaging laser targeting system (RuAF).

The earlier PNA-B attack radar was replaced with an improved Leninets PNA-D, which includes Doppler beam sharpening and terrain avoidance modes for low level penetration, there are no reports of the Sopka Terrain Following Radar (TFR) used in the Tu-160 fitted to Backfires. The SMKRITs (RORSAT Targeting Datalink Receiver) is fitted, using a Molniya satcom link. The Groza OBP-15T TV remote optical bombsight common to the Tu-160 was

The centreline Kh-22 store is carried semi-conformally, with sculpted bomb bay doors to accommodate the weapon. The bomb bay rotary launcher is otherwise used for a range of weapons (US DoD).

Outboard glove station BD-45K/F adaptors are used to carry a pair of external Kh-22 rounds, but can be replaced with bomb racks for up to 3 tonnes of free fall bombs. (via Wikipedia).

The weapons suite for the Backfire C reflects its late Cold War Soviet tasking. The primary weapon for AV-MF naval Backfires were anti-shipping, anti-radiation and nuclear variants of the very formidable Raduga Kh-22 Burya / AS-4 Kitchen [More ...]. Anti-radiation and nuclear variants were also carried by Dal'naya Aviatsia Backfire C aircraft as defence suppression weapons. The Backfire bomb bay can be fitted with doors which have contoured recesses to fit a centreline conformal Kh-22 round on a BD-45F adaptor. Two external rounds can be carried on BD-45K adaptors, mounted on the outboard glove hardpoints.

The Kh-15 / AS-16 Kickback is the Russian equivalent to SAC's AGM-69 SRAM. Note the maritime strike CONOPS using offboard targeting provided by the Tu-95RTs Bear D Uspekh / Big Bulge X-band surveillance and targeting radar (via

The bomb bay can also be fitted with an MKU series rotary launcher for six Kh-15 / AS-16 Kickback nuclear or conventional armed defence suppression missiles, a Soviet analogue to the US AGM-69A SRAM carried by the FB-111A and B-52H. Four additional rounds can be carried on the outboard glove stations, and inboard ventral inlet tunnel stations, for a total of 10 weapons.

Like US heavy bombers in the era predating precision bombs, the Backfire C can also carry a large payload of dumb bombs. External beam ejector racks can be fitted to the outboard glove stations and inboard ventral inlet tunnel stations, each carrying 9 x FAB-250 500 lb dumb bombs, which including the 24 round bomb bay stations permits carriage of up to 69 FAB-250 rounds, more than the Mk.82 payload of the B-52H. The external stations can also be used to carry paired FAB-1500 3,000 lb dumb bombs, for a total of 8 rounds. The maximum weapons payload is usually cited at 24 tonnes.

In terms of performance the Backfire C is best described as a 124 tonne 'oversized F-111', carrying around 120,000 lb of internal fuel, with Mach 2 class dash speed and a combat radius between 2,000 and 2,500 nautical miles, subject to weapon payload and profile. Eastern European sources claim that low level penetration profiles can be flown, in addition to the 'classical' high altitude supersonic profile. Tupolev data indicates that the aircraft is compatible with any runway capable of supporting a later 767 variant.

The Tu-22M3 remained in production until 1993, and various sources claim that up to 268 units were built. As IOC was achieved in 1989 and operational flying rapidly curtailed after 1991, the average number of fatigue hours accumulated by the Backfire C fleet is very low, especially for the last aircraft built, which have a calendar age of only 14 years. US sources currently put Russian Air Force inventory numbers at 105, Russian Naval Aviation numbers at 105, and Ukrainian Air Force numbers at 14 (with 16 Backfire B).


Automatic Fuel Balance Management System
Navigation System
Low Altitude Radar Altimeter (Dual)
Radio Altimeter
Doppler Nav
UHF Comm
HF Comm

Leninets PNA-D
Attack Radar
RORSAT Targeting Datalink Receiver (Molniya satcom)
Remote Optical Bombsight
Strike Camera

Avtomat 3
Radar Warning Receiver (Ural suite)
Defensive ECM (Ural suite)
ECM Automatic Noise Generator (Ural suite)
L-082 MAK UL
IR Missile Approach Warning System (Ural suite)
Chaff/Flare Dispenser (Ural)
PRS-4KM Kripton
Tail Warning/Fire Control Radar
Tail Warning/Fire Control TV System

Table 1: Tu-22M3 Baseline Avionics/Systems (Stolar/Gordon/Rigmant)


1 x Kh-22
Centreline ASCM on BD-45F Adaptor
2 x Kh-22
Outboard ASCM on BD-45K Adaptors
6 x Kh-15
ASCM on rotary launcher
4 x Kh-15
ASCM external stations
6-8 x Kh-55/65
ALCM external stations
1 x GSh-23
UKU-9A-802 barbette gun / 1200 rounds

Weapons Adaptor Kh-22 Centreline
Weapons Adaptor Kh-22 Wing Glove
Weapons Adaptor
Weapons Adaptor
Weapons Adaptor
Weapons Adaptor
Weapons Adaptor

69 x FAB-100
250 lb dumb bomb
69 x FAB-250
500 lb dumb bomb
42 x FAB-500
1,000 lb dumb bomb
8 x FAB-1500
3,000 lb dumb bomb
2 x FAB-3000
6,000 lb dumb bomb
24 x FAB-500/8 x FAB-1500
1,000 lb/3,000 lb dumb bomb
24 x FAB-500/1 x Kh-22
1,000 lb dumb bomb/ASCM
42 x 500 kg naval mines
8 x 1500 kg naval mines

Table 2: Tu-22M3 Baseline Weapons (Stolar/Gordon/Rigmant)

he Backfire sits between the F-111 and B-1B in sizing and capability, and with likely future weapons upgrades will provide similar capabilities (Author).

This chart compares the strategic punch of the Backfire against tanker supported F-111s. To strategically balance a dozen Backfires requires two dozen F-111s and a dozen supporting KC-30B/A330-200MRTT tankers. Without the F-111, the number of F/A-18As or JSFs is effectively doubled, and tanker demands are nearly doubled. Should useful numbers of Backfires arrive in the region, the current plan for the RAAF's force structure will result in a strategically irrelevant RAAF strike capability (Author).

Backfire C Growth Paths

Sources in Eastern Europe observe that the Russian Air Force has planned for some time to equip the Backfire C with a conventional precision weapons capability, emulating the current trend pursued with the US heavy bomber fleet. There are no reports as yet that this has materialised, due to the parlous budgetary situation the Russians face. With experience from the glass cockpit Su-27SKM and more recent Su-35BM MLU package design, there would be no issues for Russian designers in retrofitting a glass cockpit.

It is very unlikely that Russia would agree to export the Kh-55 / AS-15 Kent strategic cruise missile or the Kh-15A/R/S / AS-16 Kickback or SRAM-ski as part of an export package, although an anti-ship Kh-65 has been offered for export. It is known that the PLA acquired samples of the Kh-55SM via the Ukraine earlier in the decade.

Conventional variants of the Kh-22 were apparently offered to India and would not present any major issues for export. Indeed, as the PLA-AF and PLA-N both operate variants of the Styx/Silkworm which use a closely related rocket engine and the same propellants, the Kh-22 would be very easy for the PLA to support and operate. We should not be surprised if the PLA opts to licence build the Kh-22 as it could be rapidly assimilated given the infrastructure to manufacture the C-601/611. The Kh-22 remains a formidable anti-shipping weapon and with precision guidance, an extremely potent land attack weapon.

Integration of the 1,000 lb KAB-500L and 3,000 lb KAB-1500L Paveway-ski laser guided bombs would be relatively simple, exploiting hardware for the FAB-1500. Adaptation of the existing nine round FAB-250 rack to carry six KAB-500 is feasible. A thermal imaging laser targeting pod like the Sapsan-E could be carried externally, but also repackaged into the existing bombsight fairing under the flight deck, exploiting the extant Weapons Officer's display for the remote OBP-15T bombsight. The latter arrangement offers lower drag and a better field of regard, but would require additional infra-red transmissive window integration, yielding similar packaging to the JSF EOTS. Such as arrangement is likely to be attractive as it doubles up as a day/night thermal imaging sight to replace the OBP-15T, and with further integration via a HUD could provide a night penetration capability.

Clearance of the fire-and-forget KAB-500/1500Kr GBU-8-ski would present little difficulty, but inflight retargeting would require wiring additions to the glove and ventral inlet stations. The KAB-1500TK GBU-15-ski would require integration of the APK-9 Tekon pod, already carried by the Su-30MKK and Su-27SKU.

The new GPS/Glonass aided inertially guided KAB-500S-E 'JDAM-ski' based on the KAB-500 kit is currently being integrated on the Su-27SKM, Su-30MK and Su-35BM, with KAB-1500S-E integration now planned. These weapons would require software and wiring changes to integrate, and would essentially replicate the capabilities of the JDAM on US heavy bombers.

There are no fundamental obstacles to integrating the KAB family weapons on the Backfire C, and the prospect of the PLA funding such prior wishlist developments is likely to be very attractive to the cash strapped RuAF. Arguably this may have been the motivation behind senior RuAF officers publicly advocating the export of the Backfire to China.

Indian sources claimed that the integration of the Kh-31/AS-17 Krypton series, adopted by the PLA-AF for the Su-30MKK, was a likely prospect for the planned and later cancelled Indian Backfire C lease. As an inventory weapon for the PLA-AF, it is another likely development. Similar claims were also made for the Kh-35U Kharpunski, and it also could be integrated for tandem carriage on suitable launchers. A variant of the existing bomb rack fitted with tandem AKU-58 launchers would easily accommodate both the Kh-31 and Kh-35U in a low drag configuration.

It is to be expected that the PLA-AF would seek to carry its planned ALCMs on the Backfire C. As these weapons are similar in size and weight to the FAB/KAB-1500 series, a similar external carriage arrangement is to be expected. As the Chinese weapons will have unique software requirements, it would likely be a later rather than earlier addition to any export aircraft.

The PLA-AF already operates the podded L-005 Sorbtsiya and it is likely that a block upgrade of the SPS-171/172 jammer would be performed to bring them to a similar configuration. This would provide considerable commonality in the support base, and in programming jamming modes into the embedded firmware.

If a laser targeting system is fitted, there will be little near term pressure to upgrade the attack radar system. The current state of Russian multimode radar development is best exemplified by the Leninetz B004 phased array in the Su-34 Fullback, and the Tihkomirov NIIP BARS and newer Irbis E in the Su-30MK/35BM Flankers, all of which have Ground/Maritime Moving Target Indicator and Synthetic Aperture Radar high resolution mapping capabilities. A block upgrade of the PNA-D signal and data processors vs replacement with a derivative Su-30 radar would present an interesting dilemma for PLA-AF planners. The stabilised gimbal and large radome volume present considerable flexibility for retrofits. Of the choices available, the most ambitious would clearly involve integrating a gimballed variant of the Fullback's B004.

It is abundantly clear that the PLA-AF would have a wide range of options in avionic block upgrades and weapons upgrades for the Backfire C.

Above: The four crew members sit on ejection seats as in the B-1B, with individual hatches, an arrangement not unlike the F-111 (RuAF). The conventional instrumentation in the cockpit reflects the late Soviet era design heritage of the Backfire. A glass cockpit upgrade following the Su-27SKU model is a feasible option. Below: Admiral Charles R. Larson, Commander in Chief, US Pacific Fleet, sits in the cockpit of a Soviet Tu-22M Backfire aircraft during a visit to a Soviet air base during the latter Cold War period (US DoD).

Above: Aft Offensive and Defensive Systems Operator stations. Below: crew access hatches (via

A nine station MER is used to carry the 500 lb class FAB-250 demolition bomb.


The Kh-22 Burya was a contemporary of the Avro Blue Steel Mk.1 carried by Victors and Vulcans of RAF Strike Command. The Soviet missile was however larger, faster and longer ranging, and evolved across a range of roles and missions unlike the British missile, limited to nuclear strike

Avro Blue Steel Mk.1 (Image via Wikipedia).

Avro Blue Steel Mk.1 and Avro Vulcan.

Launch of a Blue Steel Mk.1 from an RAF V-bomber.

Tu-22M3 Backfire C MAKS 2005
Tupolev Bureau Images

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PostSubyek: Re: Calon Bomber Pengebug yg sgt diminati RI jika jd HIGHPROFILE postur pertahanan   Fri Sep 17, 2010 9:06 pm

Sekedar pembanding aja dr kelas yg hampir sama

Rockwell B-1 Lancer

The Rockwell (now part of Boeing) B-1 Lancer is a four-engine, variable-sweep wing strategic bomber used by the United States Air Force. First envisioned in the 1960s as a supersonic bomber with sufficient range and payload to replace the Boeing B-52 Stratofortress, it developed primarily into a low-level penetrator with long range and supersonic speed capability.

The bomber's development was delayed multiple times over its history, as the theory of strategic balance changed from flexible response to mutually assured destruction and back again. The initial B-1A version was developed in the early 1970s, but its production was canceled and only four prototypes were built. In 1980, the B-1 resurfaced as the B-1B version with the focus on low-level penetration bombing. The B-1B entered service with the United States Air Force (USAF) in 1986.

The B-1B began service with the USAF Strategic Air Command as a nuclear bomber. In the 1990s, it was converted to conventional bombing use. It was first used in combat during Operation Desert Fox in 1998 and during the NATO action in Kosovo the following year. The B-1B continues to support U.S. and NATO military in Afghanistan and Iraq. The Lancer is the supersonic component of the USAF's long-range bomber force, along with the subsonic B-52 and Northrop Grumman B-2 Spirit. The bomber is commonly called the "Bone" (originally from "B-One"). With the retirement of the General Dynamics/Grumman EF-111A Raven in 1998 and the Grumman F-14 Tomcat in 2006, the B-1B is the U.S. military's only active variable-sweep wing aircraft.


In December 1957, the U.S. Air Force selected North American Aviation's proposal to replace the Boeing B-52 Stratofortress. This would lead to the B-70 Valkyrie.[3] The Valkyrie was a six-engine bomber that could reach Mach 3 speeds at high altitude (70,000 feet / 21,000 m)[4] to avoid interceptor aircraft, the only effective anti-bomber weapon in the 1950s.[5] Soviet interceptors were unable to intercept the high-flying Lockheed U-2;[6] the Valkyrie was to fly at similar altitudes and much higher speeds.[5] By the late 1950s, however, anti-aircraft surface-to-air missiles (SAMs) could threaten high-altitude aircraft,[7] as demonstrated by the 1960 downing of Gary Powers' U-2.[8]

The USAF Strategic Air Command (SAC) began moving to low-level penetration before the U-2 downing. This tactic greatly reduces radar detection distances due to terrain masking.[9] At that time SAMs were ineffective against low-flying aircraft.[9][10] Also during the era, low flying aircraft were difficult to detect by higher flying interceptors since their radar systems could not readily pick out the aircraft due to clutter from ground reflections. Operations at low levels would limit the B-70 to subsonic speed, while dramatically decreasing its range due to higher drag.[7] The result would be an aircraft with similar speed but less range than the B-52 it was meant to replace. Unsuited for this new role and due to a growing intercontinental ballistic missile (ICBM) force, the B-70 bomber program was canceled in 1961 by President Kennedy,[5][11] and changed to a supersonic research program with two XB-70 prototypes.[12]

Although never intended for the low-level role, the B-52's flexibility allowed it to outlast its intended successor as the nature of the air war environment changed. The B-52's large airframe with internal room allowed the addition of improved electronic countermeasures suites.[13] During the Vietnam War the concept that all future wars would be nuclear was turned on its head, and the "big belly" modifications increased the B-52's bomb load to 60,000 pounds (27,215 kg),[14] turning it into a powerful tactical aircraft as well. In spite of its flexibility, the B-52 was far from perfect; higher speed would aid even a low-level approach in the strategic role, something the F-111 took advantage of.


The B-1 has a blended wing body configuration, with variable-sweep wing, four turbofan engines, and triangular fin control surfaces. The wings can sweep from 15 degrees to 67.5 degrees (full forward to full sweep). Forward-swept wing settings are used for takeoff, landings and high-altitude maximum cruise. Aft-swept wing settings are used in high subsonic and supersonic flight.[63] The wings of the B-1B originally were cleared for use at settings of 15, 25, 55 and 67.5 degrees. The 45-degree setting was later cleared in 1998–99 timeframe. The B-1's variable-sweep wings and thrust-to-weight ratio provide it with better takeoff performance, allowing it to use more runways than previous bombers.[64] The length of the aircraft presented a flexing problem due to air turbulence at low altitude. To alleviate this, Rockwell included small triangular fin control surfaces or canards near the nose on the B-1. The B-1's Structural Mode Control System rotates the canards automatically to counteract turbulence and smooth out the ride.[65]Unlike the B-1A, the B-1B made no attempt at Mach 2+ speeds. Its maximum speed is Mach 1.25 (about 950 mph or 1,530 km/h at altitude),[66] but its low-level speed increased to Mach 0.92 (700 mph, 1,130 km/h).[58] Technically, the current version of the aircraft can exceed its speed restriction, but not without risking potential damage to its structure and air intakes. To help lower its radar cross section (RCS), the B-1B uses serpentine air intake ducts and fixed intake ramps, which limit its speed compared to the B-1A. Vanes in the intake ducts serve to deflect and shield radar emissions from the highly reflective engine fan blades The B-1A's engine was modified slightly to produce the GE F101-102 for the B-1B, with an emphasis on durability, and increased efficiency.[68] The core of this engine has since been re-used in several other engine designs, including the GE F110 which has seen use in the F-14 Tomcat, F-15K/SG variants and most recent versions of the F-16 Fighting Falcon.[69] It is also the basis for the non-afterburning GE F118 used in the B-2 Spirit and the U-2S.[69] However its greatest success was forming the core of the extremely popular CFM56 civil engine, which can be found on some versions of practically every small-to-medium sized airliner.[70] The nose gear cover door has controls for the auxiliary power units (APUs), main gear doors and nearby entry ladder.[71] Controls there allow for quick starts of the APUs upon order to scramble.[72]

The B-1's offensive avionics include the Westinghouse (now Northrop Grumman) AN/APQ-164 forward-looking offensive passive electronically scanned array radar set with electronic beam steering (and a fixed antenna pointed downward for reduced radar observability), synthetic aperture radar, ground moving target indicator (MTI), and terrain-following radar modes, Doppler navigation, radar altimeter, and an inertial navigation suite.[73] The B-1B Block D upgrade added a Global Positioning System (GPS) receiver beginning in 1995.[74] The B-1's defensive electronics include the Eaton AN/ALQ-161A radar warning and defensive jamming equipment,[75] has three antennae; one at the front base of each wing and the third rear-facing in the tail radome.[76] The ALQ-161 is linked to a total of eight AN/ALE-49 flare dispensers located on top behind the canopy, which are handled by the AN/ASQ-184 avionics management system.[77] Each AN/ALE-49 dispenser has a capacity of 12 MJU-23A/B flares. The MJU-23A/B flare is one of the world's largest infrared countermeasure flares at a weight of over 3.3 pounds (1.5 kg).[78] The B-1 has also been equipped to carry the ALE-50 Towed Decoy System.[79]

Also aiding the B-1's survivability is its relatively low radar cross-section (RCS). Although not technically a stealth aircraft in a comprehensive sense, thanks to the aircraft's structure, serpentine intake paths and use of radar-absorbent material its RCS is about 1/50th that of the B-52 (probably about 26 ft² or 2.4 m²), although the Lancer is not substantially smaller in mass than the Stratofortress

Specifications (B-1B)
B-1B cockpit

Data from USAF Fact Sheet,[79] Jenkins,[140] Pace,[58] Lee[75] except where noted

General characteristics

* Crew: 4 (aircraft commander, copilot, offensive systems officer and defensive systems officer)
* Payload: 125,000 lb (56,600 kg) ; internal and external ordnance combined
* Length: 146 ft (44.5 m)
* Wingspan:
o Extended: 137 ft (41.8 m)
o Swept: 79 ft (24.1 m)
* Height: 34 ft (10.4 m)
* Wing area: 1,950 ft² (181.2 m²)
* Airfoil: NA69-190-2
* Empty weight: 192,000 lb (87,100 kg)
* Loaded weight: 326,000 lb (148,000 kg)
* Max takeoff weight: 477,000 lb (216,400 kg)
* Powerplant: 4× General Electric F101-GE-102 augmented turbofans
o Dry thrust: 14,600 lbf (64.9 kN) each
o Thrust with afterburner: 30,780 lbf (136.92 kN) each
* Fuel capacity, optional: 10,000 U.S. gal (38,000 L) fuel tank for 1–3 internal weapons bays each


* Maximum speed:
o At altitude: Mach 1.25 (721 knots, 830 mph, 1,340 km/h at 50,000 ft/15,000 m altitude)
o At low level: Mach 0.92 (700 mph, 1,130 km/h at 200–500 ft/60-150 m altitude)
* Range: 6,478 nmi (7,456 mi, 11,998 km)
* Combat radius: 2,993 nmi (3,445 mi, 5,543 km)
* Service ceiling: 60,000 ft (18,000 m)
* Wing loading: 167 lb/ft² (816 kg/m²)
* Thrust/weight: 0.38


* Hardpoints: six external hardpoints for 50,000 lb (22,700 kg) of ordnance (use for weapons currently restricted by START I treaty[87]) and 3 internal bomb bays for 75,000 lb (34,000 kg) of ordnance.
* Bombs:
o 84× Mk-82 AIR inflatable retarder general purpose bombs[141]
o 81× Mk-82 low drag general purpose bombs[142]
o 84× Mk-62 Quickstrike sea mines[143]
o 24× Mk-65 naval mines[144]
o 30× CBU-87/89/CBU-97 Cluster Bomb Units (CBU)[N 1]
o 30× CBU-103/104/105 Wind Corrected Munitions Dispenser
o 24× GBU-31 JDAM GPS guided bombs[N 2]
o 15× GBU-38 JDAM GPS guided bombs (Mk-82 general purpose warhead)[N 3]
o 24× Mk-84 general purpose bombs
o 12× AGM-154 Joint Standoff Weapon
o 96× or 144× GBU-39 Small Diameter Bomb GPS guided bombs[N 4] (not fielded on B-1 yet)
o 24× AGM-158 JASSM
o 24× B61 thermonuclear variable-yield gravity bombs[144] (no longer carried)
o 24x B83 nuclear bomb[144] (no longer carried)


* 1× AN/APQ-164 forward-looking offensive passive phased-array radar
* 1× AN/ALQ-161 radar warning and defensive jamming equipment
* 1× AN/ASQ-184 defensive management system
* 1× Lockheed Martin Sniper XR targeting pod (optional)[145][146]

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PostSubyek: Re: Calon Bomber Pengebug yg sgt diminati RI jika jd HIGHPROFILE postur pertahanan   Sat Sep 18, 2010 10:55 am

ya walaupun sebagai pembanding tp pasti ga mgkin dijual ke indonesia hehehehehe maho maho
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