S-61 (HSS-2) Part II

 

 

 

 

 

Production History

 

The Sikorsky model designation for the HSS-2 is the S-61. Since 1959, Sikorsky Aircraft has produced 794 aircraft based on the original S-61. At the end of twenty years production, Sikorsky produced the last S-61 in 1980.  Sikorsky licensees in Great Britain, Japan, Canada, and Italy have produced an additional 679. It is estimated that S-61s have flown more than 24 million hours in military service and civil use. 

 

 

 

Estimated 24 Million Flight Hours over 51 Years

 

 

Sikorsky Production by Type

 

 

Sikorsky No

Design

Quantity

S-61B

XHSS-2

10

S-61B

HSS-2

245

S-61B

CHSS-2

41

S-61B

HSS-2Z

8

 

Sub-total

304

 

 

 

S-61A

CH-3B

3

S-61A

S-61A

52

S-61D

YSH-3D

4

S-61D

SH-3D

96

S-61D

VH-3D

11

S-61D

S-61D

15

 

Sub-total

181

 

 

 

S-61R

CH-3C

74

S-61R

CH-3E

45

S-61R

HH-3E

14

S-61R

HH-3F

40

 

Sub-total

173

 

 

 

S-61L

S-61L

13

S-61N

S-61N

123

 

Sub-total

136

 

 

 

 

Total

794



 

 

 

 

 

 

1

 

 

Related Models

 

 

Sikorsky developed a series of derivatives based on the S-61 (HSS- 2.) These models are summarized below.

 

First was the S-61L in 1961 designed with a longer fuselage without sponsons for commercial passenger transport. This was followed by the S61N in 1962, retaining the sponsons for overwater transport such as offshore oil rig service.

 

On the military side Sikorsky developed the S-61R in 1963 with a fuselage modified to accommodate a rear loading ramp. U.S. Air Force ordered these aircraft designated the CH-3C to support “Texas Tower” offshore radar sites.  A later more powerful variant, the HH-3E known as the “Jolly Green Giant, saw wide and excellent service in search and rescue missions. The HH-3E featured in-flight refueling equipment permitting the first non-stop helicopter flight across the Atlantic Ocean, from New York to Paris, in 1967. U. S. Coast Guard purchased HH3F “Pelicans” with a nose radar antenna radome.  S-61R derivatives have operated in the military services of Argentina, Italy and Tunisia.

 

Another HSS-2 derivative was the S-67 Blackhawk gunship. This was a Sikorsky developed aircraft with a streamlined fuselage, main rotor head and blade modifications for high speed, and speed brakes mounted on wing trailing edges to enhance maneuverability. Begun in 1969, first flight was in August of 1970. In 1974, with a ducted fan replacing the conventional tail rotor, the S67 reached a speed of 230 mph. The S67 did not enter production.

 

 

 

VH-3D Approaching the White House South Lawn

 

 

By far, the most familiar HSS-2 derivative is the Marine Helicopter Squadron One (HMX-1) Executive Flight Detachment VH-3D Marine One helicopter with its distinctive white top. (The white tops date from HMX-1’s  S58’s first used in the Eisenhower administration. Without air conditioning, the original white tops were intended to deflect heat for a cooler interior.) The VH-3’s featured communication equipment, executive furnishings, and air conditioning tailored to the mission. An upgraded derivative, the VH-3D, continues this proud service today.

 

This aircraft transports the President of the United States, other members of the Executive Branch, and other VIP’s. Sikorsky delivered the first VH-3A’s in 1962.

They featured communication equipment, executive furnishings, and air conditioning tailored to the mission. An upgraded derivative, the VH-3D, continues this proud service today.

 

 

 

 

President Kennedy boarding a VH-3D for the first time - May 8, 1962


 

Notable Accomplishments for Sikorsky S-61 Series

 

 

1959

SH-3A

First single rotor helicopter with 5 blades
First helicopter with automatic blade fold
First to be able to simultaneously hunt and kill submarines (dipping sonar + torpedoes)

 

 

 

1960

 S-61L

First helicopter designed specifically for airline use

 

 

 

1961

SH-3A

Set world’s speed record for helicopters:

  • 3 km sea level speed record (192.9 mph)
  • 100 km speed record (183 mph)
  • 500 km speed record (179.5 mph)
  • 1,000 km speed record (175 mph)

 

 

 

1961

SH-3A

First deliveries to U.S. Navy

 

 

 

1961

S-61L

World's first multi-turbine helicopter certified for passenger transport.

 

 

 

1961

Mod SH-3A

Set new speed records (with sponsons removed):

  • 3 km sea level speed record (198.8 mph)
  • 25 km speed record (210.6 mph)

 

 

 

1962

S-61L & N 

First civil helicopters certified as IFR transports

 

 

 

1962 VH-3A Presidential transport helicopters delivered
     
1965 S-61R First helicopter operational in-flight refueling
     
1965 S-61F Experimental compound version achieves 204 knots (6 bladed rotor, two J69 jets)
     
1965 SH-3A

Record distance without landing/refueling. Flew from USS Hornet in San Diego, CA to USS
Franklin D. Roosevelt
in Jacksonville, Fla., for a distance of 2,116 st mi and average speed 126 knots

     
1965 RH-3A First flight minesweeping version
     
1967 HH-3E  First helicopter to fly non-stop across Atlantic (with 9 In-flight refuelings)
     
1969 SH-3D

Apollo 11 astronauts recovered by SH-3D “66” of squadron HS-4. The first of many such recoveries

by the SH-3D

     
1971 SH-3H SH-3H remanufacturing program initiated
     
1980   Last S-61 produced at Sikorsky after 20 years in production

 

 

Apollo 17 Recovery with USS Ticonderoga in the Background

 

Configuration Summary

 

Military

Civil

Fuselage, Landing Gear

Horiz. Tail

Tail Rotor

Sponson

Max Gross Weight

 

S-61A

Short, TW

small

small

small

19,000

SH-3A

S-61B

Short, TW

small

small

small

19,000

VH-3A

S-61V

Short, TW

small

small

small

19,000

CH-3B

 

Short, TW

small

small

small

19,500

CH-3C

S-61R

Ramp, Tri

large

small

Stub wing

22,050

SH-3D

S-61D

Short, TW

large

large

small

21,500

H/CH-3E

 

Ramp, Tri

large

small

Stub wing

22,050

HH-3F

 

Ramp, Tri

large

small

Stub wing

22,050

SH-3G

 

Short, TW

large

large

small

21,500

U/SH-3H

 

Short, TW

large

large

long

21,500

 

S-61L

Long, TW

large

small

strut

20,500

 

S-61N

Long, TW 

large

large

large

20,500

 

S-61T

Short, TW

large

large

strut

20,500

 

 

 

Definitions:

 

Short Fuselage – original design for HSS-2, SH-3A
Long Fuselage – S-61L & S-61N civil versions, 50 inches longer than short
Rear Ramp – S-61R new design with tricycle LG, 39.5 inches longer than short
Small Horizontal Tail – 20 sq ft, no strut
Large Horizontal Tail – 27 sq ft with strut
Small Tail Rotor – 10ft 4in diameter
Large Tail Rotor – 10ft, 7.25in diameter
Small Sponson – original to SH-3A, 2,200 lb displacement each
Large Sponson – used on S-61N, 3,200 lb displacement each
Long Sponson – same as small, extended aft to hold towed MAD or sonobuoys
Strut – fixed landing gear on S-61L
Stub Wing – S-61R retracts LG into sub wings on aft fuselage
TW – Tail Wheel
Tri - Tricycle

 

 

Propulsion Summary

 


Military

Civil

Engine

Continuous HP per Engine

Max HP per Engine

MGB HP Limit

SH-3A

S-61A

T58-GE-8B

1,050

1,250

2,300

VH-3A

S-61V

T58-GE-8B

1,050

1,250

2,300

CH-3B

 

T58-GE-8B

1,050

1,250

2,300

CH-3C

S-61R

T58-GE-5

1,400

1,500

2,500

SH-3D

S-61D

T58-GE-10

1,250

1,400

2,500

VH-3D

 

T58-GE-400

1,400

1,500

2,500

H/CH-3E

 

T58-GE-5

1,400

1,500

2,500

HH-3F

 

T58-GE-5

1,400

1,500

2,500

SH-3G

 

T58-GE-10

1,250

1,400

2,500

U/SH-3H

 

T58-GE-402

1,400

1,500

2,500

 

S-61L

CT58-110

1,050

1,250

2,300

 

S-61N

CT58-140

1,400

1,500

2,500

 

S-61T

CT58-140

1,400

1,500

2,500



Definitions:

 

HP – Horse Power
MGB – Main Gear Box

 

Note on US Naval Aircraft Designations.


The first S61 model carried the US Navy designation HSS-2. H for helicopter, first S for antisubmarine, second S for Sikorsky, and -2 denoting the second model in the series, since the HSS-2 was preceded by the S-58 HSS-1. In 1962 Navy modified their designation pattern so that the HSS-2 became the SH-3, with S for antisubmarine and H for helicopter.

 

Additional Information Sources

 

Information on mid-20th-century anti-submarine warfare was obtained from:  The Third Battle: Innovation in the U.S. Navy's Silent Cold War Struggle with Soviet Submarines, March 2000, by Owen Cote Jr., Director, MIT Security Studies Program, to whom the author is most grateful.

 

Color photos were obtained from the extensive Wikipedia files for the Sikorsky SH-3 Sea King, Sikorsky S-61R, Sikorsky VH-3, and Sikorsky S61L, for which the author is most grateful.

 

 

go to S-61 (HSS-2) Part I

Prepared by Jim Bohan & Tom Lawrence
Date prepared: January 31, 2012

 

 

 

 

 

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lastpdate SEPTEMBER 11, 2012