Bell AH-1T Improved SeaCobra

 

 
 
Overview
Parent type Model 209/AH-1 Cobra
Variant *No Variant assigned
Design authority Bell Helicopter Textron, Inc.
Primary manufacturer Bell Helicopter Textron, Inc.
Key Characteristics
Operational status Status unknown
Max gross weight (ground) 6,350 n/a 6,350 n/a
Crew 2
Seating arrangement Tandem
Configuration
VTOL type Helicopter
Compound type None
Lift configuration Single main rotor
Control device type Tail rotor
Features
Number of engines 2
Number of propulsors 0
Number of lift devices 1
Number of control devices 1
Milestones associated with the Bell AH-1T Improved SeaCobra
1976 First flight of the Bell AH-1T Sea Cobra

Bell AH-1T Improved SeaCobra

 

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Bell AH-1T Improved SeaCobra

 

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Bell AH-1T Improved SeaCobra

 

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Bell AH-1T Improved SeaCobra

 

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Bell AH-1T Improved SeaCobra

 

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Bell AH-1T Improved SeaCobra

 

Operated By
United States Marine Corps No longer flying

Bell AH-1T Improved SeaCobra

 

Forum Proceedings related to the Bell AH-1T Improved SeaCobra

Testing of the Tow Missile-Configured AH-1T Helicopter
Cash, Daniel G., Naval Air Test Center

 

 

Vertiflite articles related to the Bell AH-1T

Vertiflite, November/December 1985

In Production: The Marines' AH-1T + SuperCobra -

 

 

Content from the AHS website related to the Bell AH-1T

 

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Articles from the Journal of the American Helicopter Society related to the Bell AH-1T

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Articles from NASA Technical Reports Server related to the Bell AH-1T

 

Patent information from the US Patent and Trademark Office related to the Bell AH-1T

 

Google Books related to the Bell AH-1T

Bell AH-1T Improved SeaCobra

 

Overview

 

 

Bell AH-1T Improved SeaCobra

Aircraft Notes

Ref. Author(s) Title Source Date Type