High Gallery 

 

 

U. S. Military Aircraft

Grumman S-2 MOHAWK

Photo by Salamander

The Mohawk was designed to meet combined US Army and US. Marine Corps requirements of the mid 1950s for a battlefield surveillance plane. The type first flew in prototype from April 1959, offering high survivability though features such as aluminum armor, bulletproof windscreens, and flak curtains on fore and aft bulkheads, to gather with very considerable agility. The marines then pulled out of the program, leaving the army to order the OV-1A for optical reconnaissance with cameras and the OV-1B for electronic reconnaissance with side looking airborne radar and span increased by 6 ft. The Mohawk proved its capabilities in the Vietnam War, where some aircraft were fitted with hard points for four light armament. This capability was rarely used, however for the Mohawk real utility lies in its reconnaissance facility, which is much improved and diversified in later variants. total production was 329 aircraft. 

 

 

TECHNICAL DATA

Description Specifications
Manufacturer: Grumman Length: 41 ft. 0 in.
First Flight: April, 1959 Height: 12 ft. 8 in.
Model: D Wing Span: 48 ft. 0 in.
Crew: Two Wing Area: 360.0 sq. ft.
Nickname: Mohawk Empty Weight: 12,054 lb.
Basic Role: Multi sensor reconnaissance and observation plane. Max. Weight: 18,109 lb.
Other Versions: OV-1A optical reconnaissance model. OV-1B radar reconnaissance model. OV-1C a OV-1A development with an infra red surveillance system. OV-1D multi sensor variant able to accept infra red, radar, or other sensors. RV-1C and RV-1D aircraft modified permanently for electronic reconnaissance.
EV-1E aircraft modified for electronic intelligence gathering.
Armament: Generally none.
Principal User: Israel and USA

Propulsion

Performance

Power Plant: Lycoming T53-L-701 turboprops.
Range: 1,011 miles. Horsepower: 1,400-shp.
Max. Speed: 305 mph. at 10,000 ft. No. Of Engines: Two  
Ceiling: 25,000 ft.  
Climb Rate: 3,618 ft. per minute.  

 

 

Military Aircraft Grumman Previous Next