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时间:2012-03-16 12:23来源:蓝天飞行翻译 作者:航空
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A-160  A-160 
Length  35 ft  Rotorspan  36 ft 
Gross Weight  4,300 lb  Payload Capacity  300+ lb 
Fuel Capacity  2,500 lb  Fuel Type  Gasoline 
Engine Make  6-cylinder car  Power  390 hp 

Performance:
Endurance  18 hr at 15kft  Max/Loiter Speeds  140+/0 kt 
Ceiling  28,000 ft  Radius  1,700 nm 
Takeoff Means  Hover  Landing Means  Hover 

SECTION 2 - CURRENT UA PROGRAMS
Page 16

2.2.3 Cormorant
User Service: DARPA Manufacturer: Lockheed Martin Inventory:  0 Delivered/TBD Planned Background: The Cormorant project is currently conducting a series of risk reduction demonstrations for a multi-purpose UA that is “immersible” and capable of launch, recovery, and re-launch from a submerged SSGN submarine or a surface ship. Such an U A could provide all- weather ISR&T, BDA, armed recon naissance, or SOF and specialized mission support.  In particular, the combination of a stealthy SSGN submarine an d a survivable air vehicle could introduce a disruptive capability to support future joint operations.  If the current demonstrations are successful, follow-on efforts could involve building an immersible and flyable demonstrator UA.
Characteristics:

Cormorant  Cormorant 
Length  19 ft  Wing Span  16 ft 
Gross Weight  9,000 lb  Payload Capacity  1,000 lb 
Fuel Capacity  2,500 lb  Fuel Type  JP-5 
Engine Make  TBD  Power  3,000 lb thrust 

Performance:
Endurance  3 hr  Max/Loiter Speeds  0.8M/0.5M 
Ceiling  35,000 ft  Radius  400-500 nm 
Takeoff Means  Rocket-Boosted  Landing Means  Splashdown 

 

2.2.4 DP-5X
User Service: DARPA Manufacturer: Dragonfly Pictures Inventory: 0 Delivered/TBD Planned Background: The DP-5X is planned to be an FCS Class III-compliant VTOL UA.  The program has successfully completed development and test milestones and is planning to enter initial flight demonstrations. The vehicle is modular and will facilitate reconfigurations to include or remove subsystem components. The modular design allows the aircraft to be separated into distinct modules that are man-transportable.  The DP-5X has an ample payload capacity and is designed to fit into a common HMMWV system.  The unique construction allows it to be rapidly launched by two operators. The vehicle can serve as a tactical Reconnaissance, Surveillance, and Target Acquisition (RSTA) and Communication Relay platform to the Army small unit commanders at the Battalion and below level. 
Characteristics:

DP-5X  DP-5X 
Length  11 ft  Rotor Span  10.5 ft 
Gross Weight  475 lb  Payload Capacity  75 lb 
 
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本文链接地址:无人机系统路线图 Unmanned Aircraft Systems Roadmap(27)