The T-60S project was initiated by the Sukhoi bureau in 1984 and
originally it was supposed to enter service in 2003. Very little
information is available about technical characteristics of this aircraft,
which remains to be classified by the Sukhoi Design Bureau. The project
was briefly mentioned in the OKB
Sukhoi - the semi-official history of the design bureau and its
aircraft. The book was first published in English in 1996. The text reads
(OKB Sukhoi, p. 277):
- "T-60S Intermediate Range
Bomber (Project)
-
- Various
sources indicate that Sukhoi, since the late 1980s, has had an
advanced, supersonic intermediate range "Joint Continental
Bomber" under development. Information that has surfaced to date
indicates the aircraft is to replace the Tupolev Tu-22M during the
first decade of the next century. It apparently incorporates low-observables
technology and is powered by two state-of-the-art turbofan engines in
an aft mounting above the fuselage (ala Tupolev Tu-22 Backfire).
The aircraft is quipped with canards, just
ahead of a chined delta wing. Little else has surfaced concerning this
aircraft. The status of the full-scale development is unknown."
The T-60S was briefly mentioned here and there
with a few artist impressions appearing in the press, but factual
information remains scarce. Recently an interesting article about T-60S
and other perspective Russian bomber designs appeared in the Air
International (Nov. 1998, pp. 274-278). The article suggests that
the T-60S may be a high-altitude, high-speed bomber with a lifting body
fuselage design and a swing-wing construction. It was also suggested that
the aircraft is capable of supercruise at Mach 2 and its engines are
equipped with two-dimensional thrust vectoring nozzles.
- "Although no photographs of the
T-60S are available, Piotr Butkowski (Air International correspondent
on Russian aviation) believes that the T-60S features a variable
geometry wing, flat lifting fuselage and two engines, equipped with
two-dimensional thrust vectoring nozzles. The engine air intakes are
believed to be shoulder mounted, slightly forward of the wing root.
Armament is understood to include up to six Kh-101 stealthy cruise
missiles, as well as AS-15 and AS-16 missiles, free-fall nuclear
weapons and precision guided conventional munitions."
Looking at the two
illustrations to the left it is difficult not to notice that the two
configurations have absolutely nothing in common. The early
configuration, with canards and the chined delta wing, however, is
very similar to the early S-37 fighter design (not to be confused with the
latest S-37 Berkut
technology demonstrator.) The chined delta wing and canards also remind of
the T-4 bomber design back from the 1970s and the S-21
business jet project which was design in co-operation with Gulfstream. The
resemblance, however, is very general. So, where did this idea about a
wide lifting fuselage and a variable geometry wing came from?
Sukhoi is not a
traditional Russian bomber designer - this role was usually reserved for
Tupolev. However, Sukhoi does have considerable expertise in designing
ground strike aircraft (such as Su-22, Su-24, Su-25, Su-34). The design
bureau also had one very promising bomber project in the works during the
1960s and early 1970s. This project was the T-4
supersonic, intercontinental bomber developed to counter the American XB-70
Valkyrie bomber. The aircraft was completed and successfully
test-flown but then the program was abruptly terminated in 1973. The
reasons for the termination are not very clear, some suggest that it was
due to the termination of the XB-70, others - that it was a political
decision. In any case, I think that it would be logical to look back on
T-4 and its derivatives when considering a possible configuration of
T-60S.
After seeing the Air
International illustration I immediately remembered one visually
similar development of the T-4 - the T-4MS
(also known as "200".) As you can see from the illustration,
there are some considerable similarities between this aircraft and the
illustration from Air International - a variable geometry wing, a wide
lifting fuselage, internal placement of weapons and auxiliary systems. The
idea, that Sukhoi may be drawing on its past experience with bomber
design, does not seem unreasonable.
A lifting fuselage
design is not a very common feature in aviation, especially in Russian
aviation. It would be reasonable to suppose that the idea of such a
fuselage for the T-60S did not appear in the vacuum. It just so happens
that the Myasishchev Design Bureau recently unveiled its new design for a
high-altitude passenger/cargo/surveillance aircraft, featuring a wide
lifting fuselage with two high
bypass ratio turbofans installed side by side above the rear part of the
fuselage. The aircraft is the M-60
(with a proposed GP-60D
Katun ***
cargo version) and was originally designed in 1980s and, therefore, is a
contemporary of the T-60S project. The aircraft will be powered by two
Perm PS-90A turbofan engines. It can cruise at 50,000ft (and can reach
65,500 ft) at Mach 0.7, has a range of between 5,000 and 15,000 km and can
carry a load of up to 20 t. The GP-60 is a long way from being T-60S,
nevertheless, there are some undeniable similarities.
Below is the
table of T-60S estimated characteristics. To come up with this numbers I
assumed that the T-60S is a flat lifting fuselage design that uses
turbofan engines.
Sukhoi
T-60S estimated characteristics
Type |
intermediate-range
strike/interdiction aircraft |
Powerplants |
two 23,500 kg (51,800 lb)
turbofans |
Max speed |
Mach 2.04 |
Cruising speed |
Mach 2.02 |
Max altitude |
20,000 m (65,500 ft) |
Cruising altitude |
15,000 m (49,000 ft) |
Max range |
6,000 km (3,250 nm) |
Range with max load |
2,200 km (1,200 nm) |
Weight (empty) |
32,000 kg (70,500 lb) |
MTOW |
85,000 kg (188,000 lb) |
Max load |
20,000 kg (44,000 lb) |
Wing span (extended) |
37 m (121 ft) |
Wing span (swept) |
24 m (79 ft) |
Wing angle (extended) |
70 deg |
Wing angle (swept) |
30 deg |
Length |
38 m (125 ft) |
Height |
10 m (33 ft) |
Armament |
maximum of 20,000 kg
(44,000 lb) of free fall nuclear and conventional bombs, guided
munitions, up to 8 cruise missiles, including Kh-101, Kh-55MS
(AS-15 Kent) ALCM*,
Kh-15P (AS-16 Kickback) SRAM**. |
*ALCM - air launched cruise missile
**SRAM - short range attack missile
***GP -
gruzo-passazhirsky (cargo/passenger)
|
T-60S
early configuration
T-60S
later configuration
The
early S-37 fighter project
Sukhoi
T-4 bomber

XB-70
Valkyrie

Sukhoi
S-21

T-4MS
("200")

|