Sukhoi Su-7

After Joseph Stalin's death, the Sukhoi OKB was reopened and by the summer, it began work on a swept-wing front-line fighter. The first prototype, designated S-1, was designed to use the new Lyulka AL-7 turbojet engine. It was the first Soviet aircraft to utilize the all-moving tailplane and a translating centerbody, a movable inlet cone in the air intake for managing airflow to the engine at supersonic speeds. The aircraft also had a wing sweep of 60°, irreversible hydraulically boosted controls, and an ejection seat of Sukhoi’s own design. This was dictated by the highly swept wing. Combined with poor visibility from the cockpit and the lack of an instrument landing system, operations were very difficult, especially in poor weather or airfields. In 1961–1962, Sukhoi experimented with blown flaps on S-25 but the benefit was too small to warrant implementation. JATO rockets tested on S-22-4 proved more useful and were incorporated into the Su-7BKL. Attempts to improve takeoff and landing performance eventually resulted in the variable geometry Sukhoi Su-17. The Su-7B and its variants became the main Soviet ground-attack aircraft of the 1960s. They were also widely exported (691 planes, including some trainers). However, the very short combat radius and need for long runways limited the Su-7's operational usefulness. On the other hand, despite its notoriously heavy controls, the Su-7 was popular with pilots for its docile flight characteristics, simple controls and considerable speed even at low altitudes. It also had a reputation for easy maintenance. In 1977–1986 the Su-7s remaining in Soviet service were replaced by Su-17s and MiG-27s. ==Operational history==

Egypt The Su-7 saw combat with Egypt in the 1967 Six-Day War, the subsequent War of Attrition, and saw use in the Yom Kippur War by the Egyptians to attack Israeli ground forces. India The Indian Air Force (IAF) used the Su-7 extensively in the 1971 war with Pakistan. Six squadrons, totaling 140 aircraft, flew almost 1,500 offensive sorties during the war, After the war, it was found that the aircraft had high survivability, being able to fly home safely despite receiving heavy damage. For example, Wing Commander H.S. Mangat's Su-7 was badly damaged by a PL-2 missile fired by a Pakistan Air Force F-6. The impact was so severe that half the rudder was missing, the elevators, ailerons, and flaps were severely damaged, and half the missile was stuck in the chute pipe. The pilot made it back to his base. The death of at least one Indian pilot can be attributed, at least indirectly, to poor cockpit design. A pilot had moved his seating forward to a dangerous position, "because he found the bombsight and the front gun sight easier to operate" while in that position and was killed on ejection. Indian Su-7BMKs shot down at least two Shenyang F-6s in the 1971 war, Syria Syria and Iraq both received their first SU-7s from the Soviet Union in 1968, with the Syrians receiving 25 airframes in an initial batch followed by more purchases in the lead up to the 1973 Arab-Israeli war. These Su-7s were used intensively, primarily for ground attack and support missions and were valued for their supersonic performance and hard punch, and when the war broke out, the Syrian Air Force Command - let by Major General Najr Jamil - had about 80 Fitter-As ready for combat (not counting a number of Iraqi SU-7s also based in Syria at the time). SU-7s were used intensively and especially in low level attacks which the Israelis had a lot of trouble detecting and intercepting (in comparison to the MiG-21s flying top cover for the Fitters and MiG-17s). After the war, during which the Syrians suffered considerable losses, 35 SU-7s were supplied by the Russians as replacements or extra airframes, and they would be in Syrian service until the 1990s before being phased out. ==Variants==

A total of 1,847 Su-7 and its variants were built. ;Su-7BM :Upgraded AL-7F-1 engine, upgraded fuel system with external piping on either side of the fuselage spine, fuel tanks installed in the wings, "wet" underwing hardpoints for carrying external fuel tanks, capable of carrying tactical nuclear bombs. Manufactured 1963–1965 with 290 built. ;Su-7BKL :Rough field-capable variant with skids fixed to the sides of the main landing gear, provision for two SPRD-110 JATO rockets of 29.4 kN (13,300 lbf) thrust, and twin brake parachutes. Introduced in 1965, factory designation S-22KL. Manufactured 1965–1972 with 267 built. ;Su-7BMK :A simplified export version of the Su-7BM. Manufactured 1967–1971 with 441 built. ;Su-7U (NATO Moujik) :Two-seat trainer version of the Su-7B with reduced fuel capacity. First flight 25 October 1965. Manufactured 1966–1972 in parallel with the export version, designated Su-7UMK. ;Su-7UM (NATO Moujik) :Two-seat training version of the Su-7BM. ;Su-7UMK (NATO Moujik) :Two-seat training version of the Su-7BMK. All Su-7 trainers amounted to 411 built. ;Su-7IG :Experimental variable geometry wing aircraft which was developed into Sukhoi Su-17. ;100LDU Control Configured Vehicle :A Su-7U modified with canards and a longitudinal stability augmentation system. It was designed as a testbed for a fly-by-wire system for the Sukhoi T-4. It was later used in 1973–1974 during the development of the Su-27's fly-by-wire system. OKB-51 designations ;S-1 :(Strelovidnoye [krylo] – swept wings) OKB-51 designation for the first prototype of the Su-7 / Su-9 family. ;S-2 :OKB-51 designation for the first production version of the Su-7. ;S-22 :OKB-51 designation for the Su-7B production aircraft. ;S-22-2 :OKB-51 designation for the prototype of the Su-7BM. ;S-22M :OKB-51 designation for the Su-7BM production aircraft. ;S-22KL :OKB-51 designation for the Su-7BKL production aircraft, incorporating the short field equipment tested on the S-22-4. ;S-23 :As a precursor to the S-22-4 tests, the S-23 was tested with a pure ski undercarriage and with skis on the main legs only ;S-22-4 :An S-22 tested with wheel / ski undercarriage, brake parachute and SPRD-110 JATO boosters for rough/unpaved field operations. ;S-25 :This aircraft was used for Boundary Layer Control (BLC) tests, with compressor bleed air blown over the leading edges to reduce takeoff length. ;S-25T :A Su-7 fitted with the Boundary Layer Control system, rigged especially for use in a full-scale wind tunnel. ;S-26 :A continuation of the S-22-4 testing with wheel/ski undercarriage, double brake parachute and JATO boosters (The S-26 survives on display at the Russian Air Force Museum, Monino). ;S-22MK :A simplified export version of the Su-7BKL, designated Su-7BMK ;U-22 :A belated trainer version with two seats in tandem in an extended nose based on the Su-7BM. ;U-22MK :OKB-51 designation for the export version of the Su-7U, designated Su-7UMK by the Soviet Air Force ;S-3 :A projected interceptor version of the S-2, with "Izumrud" radar and avionic equipment in a reconfigured nose section. ;S-41 :OKB-51 designation for an experimental version of the S-1/S-2 with a lengthened nose and area-ruled rear fuselage. ;T-1 :A delta-wing tactical fighter project, based on the S-2, cancelled with the prototype nearly complete. ;T-3 : A delta-winged interceptor version of the S-2, developed in parallel to the S-3 and T-1. This would eventually lead to the T-43 prototype of the Su-9 interceptor. ==Operators==

Current operators ; • North Korean Air Force – received at least 28 Su-7BMK/-7UMK in 1971. The aircraft were ordered in 1969. Former operators • Afghan Air Force – 24 Su-7BMK and 16 Su-7U trainers, were delivered to Afghanistan from 1972. Constant fighting, a high accident rate in the high altitude and poor maintenance caused substantial attrition. An additional 79 used replacements from Soviet stocks were supplied during the 1980s. None remain in service. • Algerian Air Force – 40 Su-7BMK. • Czechoslovak Air Force – the Czechoslovak Air Force was the first foreign operator of the Su-7 in 1963. Totals included 64 Su-7BM, 31 Su-7BKL and Su-7U. During operations service, 30 aircraft were lost in accidents. The remaining aircraft were phased out in 1990. • Egyptian Air Force – The first batch of 14 Su-7BMK was destroyed during the Six-Day War. From 1967–1972, Egypt received an additional 185 Su-7BMK/SU-7UMK. Those which survived the Yom Kippur War with Israel were retired in the mid-1980s. • Indian Air Force – 140 were delivered in 1968, equipping six squadrons. An additional 14 attrition replacements were provided. The last aircraft were retired in 1986. • Iraqi Air Force – The first contract for up to 34 Su-7BMK was signed in 1965, with deliveries starting in the spring of 1967. An additional order for 20 Su-7BMK was signed in July 1967. No longer in service. • Polish Air Force – operated 6 Su-7BM, 33 Su-7BKŁ and 8 Su-7U from July 1964 until June 1990; no longer in service. • Soviet Air Force • Syrian Air Force – Shortly after the Six-Day War of 1967, Syria received 25 Su-7s. During the 1973 Yom Kippur War, Syria lost most of the aircraft supplied. After 1973, The Soviet Union resupplied Syria with 35 more aircraft. By the mid 1980s, the Su-7 had been transferred to the reserves, and by the 1990s were decommissioned. ==Specifications (Su-7BKL)==