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fighting ships of the world

SOVIET / RUSSIAN NAVY (USSR / RUSSIA)

SUBMARINES

M-254 submarine (project 615) (1953)

M-255 submarines (project A-615) (1955 - 1957)

M-361 submarine (project 637)

M-321 1960

M-361

Name No Yard No Builder Laid down Launched Comp Fate
Project 615
Ì-254 [M-254]   579 196 Yd (Sudomekh), Leningrad 17.3.1950 31.8.1950 31.5.1953 training hulk 1959
Project A615              
Ì-255 [M-255]   664 196 Yd (Sudomekh), Leningrad 8.9.1953 16.9.1954 10.12.1955 stricken 3.1968
Ì-256 [M-256]   665 196 Yd (Sudomekh), Leningrad 23.9.1953 15.9.1954 21.12.1955 fire 26.9.1957
Ì-257 [M-257]   666 196 Yd (Sudomekh), Leningrad 10.11.1953 30.9.1954 10.12.1955 test hulk 2.1958
Ì-258 [M-258]   667 196 Yd (Sudomekh), Leningrad 18.11.1953 4.11.1954 21.12.1955 stricken 12.1966
Ì-259 [M-259]   668 196 Yd (Sudomekh), Leningrad 12.1.1954 5.11.1954 13.12.1955 stricken 9.1972
Ì-260 [M-260]   669 196 Yd (Sudomekh), Leningrad 14.2.1954 21.5.1955 31.7.1956 stricken 1.1970
Ì-261 [M-261], 6.1978- ÌÑ-261 [MS-261]   1070 196 Yd (Sudomekh), Leningrad 23.2.1954 21.5.1955 31.7.1956 stricken 5.1980, preserved
Ì-262 [M-262]   1071 196 Yd (Sudomekh), Leningrad 20.3.1954 12.7.1955 31.7.1956 stricken 1.1970
Ì-263 [M-263]   1072 196 Yd (Sudomekh), Leningrad 8.4.1954 2.8.1955 2.11.1956 stricken 6.1976
Ì-264 [M-264]   1073 196 Yd (Sudomekh), Leningrad 4.6.1954 14.9.1955 3.10.1956 stricken 7.1977
Ì-265 [M-265]   1074 196 Yd (Sudomekh), Leningrad 15.7.1954 9.9.1955 30.9.1956 stricken 1978
Ì-266 [M-266], 8.1977- ÌÑ-266 [MS-266]   1075 196 Yd (Sudomekh), Leningrad 30.8.1954 30.10.1955 30.9.1956 stricken 1979
Ì-267 [M-267]   1078 196 Yd (Sudomekh), Leningrad 15.10.1954 14.1.1956 30.9.1956 stricken 1980
Ì-268 [M-268]   1079 196 Yd (Sudomekh), Leningrad 20.11.1954 16.4.1956 26.12.1956 stricken 1980
Ì-269 [M-269], 8.1977- ÌÑ-269 [MS-269]   1080 196 Yd (Sudomekh), Leningrad 30.11.1954 17.3.1956 27.8.1957 stricken 1980
Ì-295 [M-295]   701 196 Yd (Sudomekh), Leningrad 10.1.1955 3.4.1956 16.8.1957 stricken 1973
Ì-296 [M-296], 8.1977- ÌÑ-296 [MS-296]   702 196 Yd (Sudomekh), Leningrad 1.2.1955 4.4.1956 23.12.1958 stricken 6.1979, preserved
Ì-297 [M-297]   703 196 Yd (Sudomekh), Leningrad 5.8.1955 29.7.1956 29.8.1957 stricken 9.1975
Ì-298 [M-298]   704 196 Yd (Sudomekh), Leningrad 2.8.1955 30.6.1956 31.8.1957 stricken 1975
Ì-299 [M-299]   705 196 Yd (Sudomekh), Leningrad 19.9.1955 4.10.1956 30.11.1957 stricken 1978
Ì-300 [M-300]   711 196 Yd (Sudomekh), Leningrad 27.9.1955 12.10.1956 30.11.1957 stricken 1976
Ì-301 [M-301]   713 196 Yd (Sudomekh), Leningrad 7.1.1956 23.2.1957 27.12.1958 stricken 1979
Ì-321 [M-321], 7.1980- ÌÑ-321 [MS-321]   715 196 Yd (Sudomekh), Leningrad 24.12.1955 23.2.1957 23.12.1958 stricken 1981
Ì-351 [M-351]   801 194 Marti Yd, Leningrad 24.3.1954 4.7.1955 3.8.1956 stricken 1974
Ì-352 [M-352]   802 194 Marti Yd, Leningrad 10.4.1954 7.10.1955 30.9.1956 stricken 5.1980
Ì-353 [M-353], 5.1978- ÌÑ-353 [MS-353]   803 194 Marti Yd, Leningrad 15.5.1955 26.4.1956 30.9.1956 stricken 1.1980
Ì-354 [M-354], 6.1979- ÌÑ-354 [MS-354]   804 194 Marti Yd, Leningrad 23.6.1955 5.6.1956 25.11.1956 stricken 1979
Ì-355 [M-355]   805 194 Marti Yd, Leningrad 8.7.1955 17.4.1957 1.8.1957 stricken 1980
Ì-356 [M-356]   816 194 Marti Yd, Leningrad 5.4.1956 27.4.1957 20.8.1957 stricken 1974
Project 637              
Ì-361 [M-361]   817 194 Marti Yd, Leningrad 5.1955 3.1957 --- never completed
  
Data variant pr. 615, A-615

Displacement standard, t

 

Displacement normal, t

pr. 615: 392 / 493

pr. A615: 406 / 504

Length, m

pr. 615: 56.6

pr. A615: 56.8

Breadth, m

pr. 615: 4.44

pr. A615: 4.46

Draught, m

pr. 615: 2.78

pr. A615: 3.59

No of shafts

3

Machinery

pr. 615: 1 32D AIP diesel + 2 M-50 diesels / 1 32D AIP diesel / 1 PG-106 electric motor for cruising

pr. A615: 1 32D AIP diesel + 2 M-50P diesels / 1 32D AIP diesel / 1 PG-106 electric motor for cruising

Power, h. p.

pr. 615: 2300 (900+2x700) / 900 / 100

pr. A615: 2700 (900+2x900) / 900 / 100

Max speed, kts

pr. 615: 17.2 / 15.4

pr. A615: 16.1 / 15

Fuel, t

diesel oil

Endurance, nm(kts)

pr. 615: 1700(9.1) / 325(2.5)

pr. A615: 3150(8.3) / 410(3.5)

Armament

pr. 615: 1 x 2 - 25/112 2M-8, 4 - 533 TT (bow, 4)

pr. A615 completed 1955-56: 1 x 2 - 25/112 2M-8, 4 - 533 TT (bow, 4)

pr. A615 completed 1956-58: 4 - 533 TT (bow, 4)

Electronic equipment

Flag radar, Tamir-5L, Mars-16KIG sonars

Complement

pr. 615: 29

pr. A615: 41

Diving depth operational, m

100

 

Data variant pr. 637

Displacement standard, t

 

Displacement normal, t

425 / 680

Length, m

58.2

Breadth, m

4.46

Draught, m

3.45

No of shafts

3

Machinery

1 32D AIP diesel + 2 M-50P diesels / 1 32D AIP diesel / 1 PG-106 electric motor for cruising

Power, h. p.

2700 (900+2x900) / 900 / 100

Max speed, kts

16 / 15

Fuel, t

diesel oil

Endurance, nm(kts)

2700(8) / 350(3.5)

Armament

4 - 533 TT (bow, 4)

Electronic equipment

Flag radar, Tamir-5L, Mars-16KIG sonars

Complement

33

Diving depth operational, m

100

Project history: This closed cycle ('single propulsion system', in Soviet parlance) design was chosen in preference to the conventional Project 612 as successor to the earlier M-classes. Project 615 was by TsKB-18; the production A615 was by TsKB-16 (the chief designer, Kassatier, apparently transferred to TsKB-16) The Kreislauf powerplant, derived from prewar experiments, ran submerged n an internal supply of liquid oxygen; oxygen was added after exhaust was passed through a lime chemical absorbent (ED KhPI). The submarine could also use a snorkel. There were three engines: one 32D diesel (900bhp) on the centre shaft, plus a pair of 700/900bhp M-50/M-50P diesels (a type used on torpedo boats), with a 100hp creep motor on the centre shaft and a back-up diesel generator aft. Boats could run at low speed using only the centreline diesel.

    Because liquid oxygen could be stored for only a limited period, the boat could not operate far from a base. To overcome this problem, in 1954-55 the Project 637 submarine was designed to use a new 'B-2 single product', consisting of solid granules containing bonded oxygen and a carbon dioxide absorbent. Exhaust gas passed through it would have its carbon dioxide leached out while its oxygen content was renewed. In 1958-59 M-361, then under oh construction, was retrofitted to test B-2, but in 1960 her trial programme was stopped and closed-cycle work ended because of the success of the nuclear programme.

Modernizations: None.

Naval service: M-256 was lost 26.9.1957 off Tallin due to fire.

Pr. A615 1970

 

© Ivan Gogin, 2015