Sikorsky Aircraft
Updated: 11/4/2025, 2:07:37 PM Wikipedia source
Sikorsky Aircraft is an American aircraft manufacturer based in Stratford, Connecticut. It was established by the Russian-American aviation pioneer Igor Sikorsky in 1923, and was among the first companies to manufacture helicopters for civilian and military use. It also produced seaplanes for passenger transport and surface vehicles such as trains and boats. Sikorsky was owned by United Technologies Corporation until November 2015, when it was sold to Lockheed Martin.
Infobox
Parent
mw- United Aircraft and Transport Corporation (1929–1934)United Aircraft Corporation (1934–1974)United Technologies (1975–2015)Lockheed Martin (2015–present)
Founded
1923; 102 years ago (1923)
Founder
Igor Sikorsky
Website
sikorsky.com
Industry
Aviation Defense industry
Products
Helicopters, other aircraft
Divisions
Sikorsky Development Flight Center, West Palm Beach, Florida, US (founded 1977)
Key people
Richard Benton (president)
Company type
Subsidiary
Headquarters
Stratford, Connecticut, United States
Subsidiaries
Schweizer Aircraft (closed 2012) PZL Mielec (now a Lockheed Martin subsidiary)Tata–Sikorsky Aerospace Limited (JV with TASL)
Number of employees
15,975 (2014)
Tables
· Products › Helicopters, production
S-47
S-47
Model
S-47
Designation
R-4
From
1942
Until
1944
MTOW (lb, t)
2,581
MTOW (lb, t)
1.17
Notes
World's first production helicopter
S-48/S-51
S-48/S-51
Model
S-48/S-51
Designation
R-5/H-5
From
1944
Until
1952
MTOW (lb, t)
4,825
MTOW (lb, t)
2.19
Notes
higher load, endurance, speed, and service ceiling than the R-4
S-49
S-49
Model
S-49
Designation
R-6
From
1945
MTOW (lb, t)
2,600
MTOW (lb, t)
1.18
Notes
improved R-4 with new fuselage
S-52
S-52
Model
S-52
Designation
H-18/HO5S
From
1947
MTOW (lb, t)
2,700
MTOW (lb, t)
1.225
Notes
all-metal rotors
S-55
S-55
Model
S-55
Designation
H-19 Chickasaw
From
1949
MTOW (lb, t)
7,500
MTOW (lb, t)
3.41
Notes
ten passenger utility, H-19 Chickasaw
S-56
S-56
Model
S-56
Designation
CH-37 Mojave
From
1953
MTOW (lb, t)
31,000
MTOW (lb, t)
14.1
Notes
twin-piston engined, H-37A Mojave
S-58
S-58
Model
S-58
Designation
H-34 Choctaw
From
1954
Until
1970
MTOW (lb, t)
14,000
MTOW (lb, t)
6.35
Notes
18 passenger larger, advanced S-55, including ASW, VIP versions
S-61
S-61
Model
S-61
Designation
SH-3
From
1959
MTOW (lb, t)
19,000
MTOW (lb, t)
8.62
Notes
medium-lift transport/airliner
S-61
S-61
Model
S-61
Designation
SH-3 Sea King
From
1959
Until
1970s
MTOW (lb, t)
22,050
MTOW (lb, t)
10
Notes
ASW, SAR or transport
S-61
S-61
Model
S-61
Designation
CH-124 Sea King
From
1963
Until
2018
MTOW (lb, t)
22,050
MTOW (lb, t)
10
Notes
Canadian Armed Forces export version
S-61R
S-61R
Model
S-61R
Designation
CH-3/HH-3
From
1963
Until
1970s
MTOW (lb, t)
22,050
MTOW (lb, t)
10
Notes
S-61 with rear cargo ramp: CH-3, HH-3 "Jolly Green Giant", and HH-3F Pelican (1963)
S-62
S-62
Model
S-62
Designation
HH-52 Seaguard
From
1958
MTOW (lb, t)
8,300
MTOW (lb, t)
3.76
Notes
amphibious helicopter
S-64 Skycrane
S-64 Skycrane
Model
S-64 Skycrane
Designation
CH-54 Tarhe
From
1962
MTOW (lb, t)
42,000
MTOW (lb, t)
19.05
Notes
"flying crane"
S-64
S-64
Model
S-64
Designation
CH-54 Tarhe
From
1962
MTOW (lb, t)
47,000
MTOW (lb, t)
21
Notes
US Army transport
S-65
S-65
Model
S-65
Designation
CH-53 Sea Stallion
From
1964
Until
1978
MTOW (lb, t)
42,000
MTOW (lb, t)
19.1
Notes
medium/heavy lift transport
S-65
S-65
Model
S-65
Designation
MH-53
From
1967
Until
1970
MTOW (lb, t)
46,000
MTOW (lb, t)
21
Notes
long-range search and rescue
S-70
S-70
Model
S-70
Designation
UH-60 Black Hawk
From
1974
Until
current
MTOW (lb, t)
23,500
MTOW (lb, t)
10.66
Notes
twin-turbine medium transport/utility, selected in 1976 for the US Army UTTAS, multiple models
S-70
S-70
Model
S-70
Designation
SH-60 Sea Hawk
From
1979
Until
current
MTOW (lb, t)
23,000
MTOW (lb, t)
10.4
Notes
US Navy anti-ship warfare, combat, SAR, support, Medevac
S-70
S-70
Model
S-70
Designation
HH-60 Pave Hawk
From
1982
Until
current
MTOW (lb, t)
22,000
MTOW (lb, t)
9.9
Notes
USAF combat, SAR, Medevac with PAVE electronics
S-70
S-70
Model
S-70
Designation
HH-60 Jayhawk
From
1990
Until
1996
MTOW (lb, t)
21,884
MTOW (lb, t)
9.93
Notes
US Coast Guard SAR and patrol
S-76
S-76
Model
S-76
From
1977
Until
current
MTOW (lb, t)
11,700
MTOW (lb, t)
5.31
Notes
twin turbine, 14-seat commercial (ex S-74)
S-80
S-80
Model
S-80
Designation
CH-53E Super Stallion
From
1974
Until
1980s
MTOW (lb, t)
73,500
MTOW (lb, t)
33.3
Notes
CH-53 derived, export version: S-80
S-92
S-92
Model
S-92
Designation
H-92 Superhawk
From
1998
Until
current
MTOW (lb, t)
27,700
MTOW (lb, t)
12.6
Notes
twin-turbine medium-lift developed from the S-70
S-92
S-92
Model
S-92
Designation
CH-148 Cyclone
From
2018
Until
current
MTOW (lb, t)
28,650
MTOW (lb, t)
13
Notes
Canadian military S-92 to replace the CH-124 Sea King
S-95
S-95
Model
S-95
Designation
CH-53K King Stallion
From
2018
Until
current
MTOW (lb, t)
84,700
MTOW (lb, t)
38.4
Notes
CH-53E Super Stallion/S-80 development
S-300C
S-300C
Model
S-300C
From
1964
Until
2018
MTOW (lb, t)
2,050
MTOW (lb, t)
0.93
Notes
three-seat single-piston, currently made by Schweizer RSG
S-333
S-333
Model
S-333
From
1992
Until
2018
MTOW (lb, t)
2,550
MTOW (lb, t)
1.16
Notes
single turbine S-300, currently made by Schweizer RSG
S-434
S-434
Model
S-434
From
2008
Until
2015
MTOW (lb, t)
3,200
MTOW (lb, t)
1.45
Notes
improved S-333
| Model | Designation | From | Until | MTOW (lb, t) | Notes | |
| S-47 | R-4 | 1942 | 1944 | 2,581 | 1.17 | World's first production helicopter |
| S-48/S-51 | R-5/H-5 | 1944 | 1952 | 4,825 | 2.19 | higher load, endurance, speed, and service ceiling than the R-4 |
| S-49 | R-6 | 1945 | 2,600 | 1.18 | improved R-4 with new fuselage | |
| S-52 | H-18/HO5S | 1947 | 2,700 | 1.225 | all-metal rotors | |
| S-55 | H-19 Chickasaw | 1949 | 7,500 | 3.41 | ten passenger utility, H-19 Chickasaw | |
| S-56 | CH-37 Mojave | 1953 | 31,000 | 14.1 | twin-piston engined, H-37A Mojave | |
| S-58 | H-34 Choctaw | 1954 | 1970 | 14,000 | 6.35 | 18 passenger larger, advanced S-55, including ASW, VIP versions |
| S-61 | SH-3 | 1959 | 19,000 | 8.62 | medium-lift transport/airliner | |
| S-61 | SH-3 Sea King | 1959 | 1970s | 22,050 | 10 | ASW, SAR or transport |
| S-61 | CH-124 Sea King | 1963 | 2018 | 22,050 | 10 | Canadian Armed Forces export version |
| S-61R | CH-3/HH-3 | 1963 | 1970s | 22,050 | 10 | S-61 with rear cargo ramp: CH-3, HH-3 "Jolly Green Giant", and HH-3F Pelican (1963) |
| S-62 | HH-52 Seaguard | 1958 | 8,300 | 3.76 | amphibious helicopter | |
| S-64 Skycrane | CH-54 Tarhe | 1962 | 42,000 | 19.05 | "flying crane" | |
| S-64 | CH-54 Tarhe | 1962 | 47,000 | 21 | US Army transport | |
| S-65 | CH-53 Sea Stallion | 1964 | 1978 | 42,000 | 19.1 | medium/heavy lift transport |
| S-65 | MH-53 | 1967 | 1970 | 46,000 | 21 | long-range search and rescue |
| S-70 | UH-60 Black Hawk | 1974 | current | 23,500 | 10.66 | twin-turbine medium transport/utility, selected in 1976 for the US Army UTTAS, multiple models |
| S-70 | SH-60 Sea Hawk | 1979 | current | 23,000 | 10.4 | US Navy anti-ship warfare, combat, SAR, support, Medevac |
| S-70 | HH-60 Pave Hawk | 1982 | current | 22,000 | 9.9 | USAF combat, SAR, Medevac with PAVE electronics |
| S-70 | HH-60 Jayhawk | 1990 | 1996 | 21,884 | 9.93 | US Coast Guard SAR and patrol |
| S-76 | 1977 | current | 11,700 | 5.31 | twin turbine, 14-seat commercial (ex S-74) | |
| S-80 | CH-53E Super Stallion | 1974 | 1980s | 73,500 | 33.3 | CH-53 derived, export version: S-80 |
| S-92 | H-92 Superhawk | 1998 | current | 27,700 | 12.6 | twin-turbine medium-lift developed from the S-70 |
| S-92 | CH-148 Cyclone | 2018 | current | 28,650 | 13 | Canadian military S-92 to replace the CH-124 Sea King |
| S-95 | CH-53K King Stallion | 2018 | current | 84,700 | 38.4 | CH-53E Super Stallion/S-80 development |
| S-300C | 1964 | 2018 | 2,050 | 0.93 | three-seat single-piston, currently made by Schweizer RSG | |
| S-333 | 1992 | 2018 | 2,550 | 1.16 | single turbine S-300, currently made by Schweizer RSG | |
| S-434 | 2008 | 2015 | 3,200 | 1.45 | improved S-333 | |
· Products › Helicopters, prototypes
S-46
S-46
Model
S-46
Designation
VS-300
Year
1939
MTOW (lb, t)
1,150
MTOW (lb, t)
0.52
Notes
first US single lifting rotor helicopter
S-50
S-50
Model
S-50
Notes
projected small helicopter; only a wooden mockup built
S-53
S-53
Model
S-53
Designation
XHJS-1
Year
1947
Notes
naval utility, two prototypes
S-54
S-54
Model
S-54
Year
1948
Notes
R-4B modified to a "sesqui-tandem" configuration
S-59
S-59
Model
S-59
Designation
XH-39
Year
1953
MTOW (lb, t)
3,361
MTOW (lb, t)
1.53
Notes
2 H-18s converted to use one turbine, 1 prototype
S-60
S-60
Model
S-60
Year
1959
MTOW (lb, t)
21,000
MTOW (lb, t)
9.5
Notes
CH-37-derived prototype "flying crane", crashed 1961
S-67
S-67
Model
S-67
Designation
Blackhawk
Year
1970
MTOW (lb, t)
24,272
MTOW (lb, t)
11
Notes
attack prototype, predecessor: S-66 AAFSS competitor
S-68
S-68
Model
S-68
Notes
proposed modification of the S-58T, none built
S-69
S-69
Model
S-69
Year
1973
MTOW (lb, t)
12,500
MTOW (lb, t)
5.7
Notes
prototype jet compound helicopter with coaxial rotors
S-71
S-71
Model
S-71
Designation
AAH
Notes
US Army Advanced Attack Helicopter entry with S-70 dynamic components
S-72
S-72
Model
S-72
Year
1976
MTOW (lb, t)
26,047
MTOW (lb, t)
11.8
Notes
NASA experimental jet hybrid
S-73
S-73
Model
S-73
Designation
HLH
MTOW (lb, t)
118,000
MTOW (lb, t)
53.5
Notes
US Army Heavy Lift Helicopter entry
S-75
S-75
Model
S-75
Year
1984
MTOW (lb, t)
8,470
MTOW (lb, t)
3.82
Notes
advanced Composite Airframe Program (ACAP) all-composite, two prototypes
S-78-20 & S-78-29
S-78-20 & S-78-29
Model
S-78-20 & S-78-29
Year
1975
MTOW (lb, t)
17,520 (-20)19,997 (-29)
MTOW (lb, t)
7.95 (-20)9.07 (-29)
Notes
proposed variation on S-70 in 20- and enlarged 29-pax models, purpose-built for commercial use. Initially designated S-70C-. Reexplored and redesignated, post S-76, but ultimately never built.
S-97 Raider
S-97 Raider
Model
S-97 Raider
Designation
AAS
Year
2015
MTOW (lb, t)
11,000
MTOW (lb, t)
4.99
Notes
US Army Armed Aerial Scout proposed compound helicopter
S-100
S-100
Model
S-100
Designation
SB>1 Defiant
Year
2019
Notes
compound helicopter prototype with rigid coaxial rotors for US Army's Future Long-Range Assault Aircraft competition
S-102
S-102
Model
S-102
Designation
Raider X
Year
2023
Notes
compound helicopter with rigid coaxial rotors for US Army's Future Attack Reconnaissance Aircraft competition
S-103
S-103
Model
S-103
Designation
Defiant X
Notes
compound helicopter with rigid coaxial rotors for US Army's Future Long-Range Assault Aircraft competition
Firefly
Firefly
Model
Firefly
Notes
electric S-300 unveiled in 2010
X2
X2
Model
X2
Year
2008
MTOW (lb, t)
6,000
MTOW (lb, t)
2.72
Notes
experimental high-speed compound helicopter with coaxial rotors
| Model | Designation | Year | MTOW (lb, t) | Notes | |
| S-46 | VS-300 | 1939 | 1,150 | 0.52 | first US single lifting rotor helicopter |
| S-50 | projected small helicopter; only a wooden mockup built | ||||
| S-53 | XHJS-1 | 1947 | naval utility, two prototypes | ||
| S-54 | 1948 | R-4B modified to a "sesqui-tandem" configuration | |||
| S-59 | XH-39 | 1953 | 3,361 | 1.53 | 2 H-18s converted to use one turbine, 1 prototype |
| S-60 | 1959 | 21,000 | 9.5 | CH-37-derived prototype "flying crane", crashed 1961 | |
| S-67 | Blackhawk | 1970 | 24,272 | 11 | attack prototype, predecessor: S-66 AAFSS competitor |
| S-68 | proposed modification of the S-58T, none built | ||||
| S-69 | 1973 | 12,500 | 5.7 | prototype jet compound helicopter with coaxial rotors | |
| S-71 | AAH | US Army Advanced Attack Helicopter entry with S-70 dynamic components | |||
| S-72 | 1976 | 26,047 | 11.8 | NASA experimental jet hybrid | |
| S-73 | HLH | 118,000 | 53.5 | US Army Heavy Lift Helicopter entry | |
| S-75 | 1984 | 8,470 | 3.82 | advanced Composite Airframe Program (ACAP) all-composite, two prototypes | |
| S-78-20 & S-78-29 | 1975 | 17,520 (-20)19,997 (-29) | 7.95 (-20)9.07 (-29) | proposed variation on S-70 in 20- and enlarged 29-pax models, purpose-built for commercial use. Initially designated S-70C-. Reexplored and redesignated, post S-76, but ultimately never built. | |
| S-97 Raider | AAS | 2015 | 11,000 | 4.99 | US Army Armed Aerial Scout proposed compound helicopter |
| S-100 | SB>1 Defiant | 2019 | compound helicopter prototype with rigid coaxial rotors for US Army's Future Long-Range Assault Aircraft competition | ||
| S-102 | Raider X | 2023 | compound helicopter with rigid coaxial rotors for US Army's Future Attack Reconnaissance Aircraft competition | ||
| S-103 | Defiant X | compound helicopter with rigid coaxial rotors for US Army's Future Long-Range Assault Aircraft competition | |||
| Firefly | electric S-300 unveiled in 2010 | ||||
| X2 | 2008 | 6,000 | 2.72 | experimental high-speed compound helicopter with coaxial rotors | |
References
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