Unmanned Aircraft Systems Roadmap 2005-2030 - Federation of ...
Unmanned Aircraft Systems Roadmap 2005-2030 - Federation of ... Unmanned Aircraft Systems Roadmap 2005-2030 - Federation of ...
UAS ROADMAP 2005 2.2.7 Eagle Eye User Service: Coast Guard Manufacturer: Bell Textron Inventory: 0 Delivered/69 Planned Background: The Coast Guard selected the Bell model TR911D Eagle Eye tiltrotor in February 2003 to serve as the cutter-based UA in its Deepwater program. The Deepwater program will begin evaluation of a prototype aircraft in 2007. Characteristics: Eagle Eye Eagle Eye Length 17 ft Rotor Span 15.2 ft Gross Weight 2,850 lb Payload Capacity 200-300 lb Fuel Capacity 832 lb Fuel Type JP/Diesel Engine Make P&W 200-55 Power 641 hp Data Link(s) LOS C2/Video LOS C2 Frequency Ku-Band/S-Band Performance: Endurance 5.5 hr Max/Loiter Speeds 210/97 kt Ceiling 20,000 ft Radius 110 nm w/3 hr TOS Takeoff Means Hover Landing Means Hover Sensor MMR Sensor Make Telephonics 1700-CG EO/IR FSI Star Safire III SECTION 2 - CURRENT UA PROGRAMS Page 19
UAS ROADMAP 2005 2.3 SPECIAL OPERATIONS UAS 2.3.1 Neptune User Service: Navy Manufacturer: DRS Unmanned Technologies Inventory: 15 Delivered/27 Planned Background: Neptune is a new tactical UA design optimized for at-sea launch and recovery. Carried in a 72x30x20 inch case that transforms into a pneumatic launcher, it can be launched from small vessels and recovered in open water. It can carry IR or color video sensors, or can be used to drop small payloads. Its digital data link is designed to minimize multipath effects over water. First flight occurred in January 2002, and an initial production contract was awarded to DRS Unmanned Technologies in March 2002. Characteristics: Neptune Neptune Length 6 ft Wing Span 7 ft Gross Weight 80 lb Payload Capacity 20 lb Fuel Capacity 18 lb Fuel Type MOGAS Engine Make 2 Stroke Power 15 hp Data Link(s) LOS C2 Frequency UHF LOS Video UHF Performance: Endurance 4 hr Max/Loiter Speeds 84/60 kt Ceiling 8,000 ft Radius 40 nm Takeoff Means Pneumatic Landing Means Water/Skid/Parachute Sensor EO or IR Sensor Make DRS SECTION 2 - CURRENT UA PROGRAMS Page 20
- Page 2 and 3: UAS ROADMAP 2005
- Page 4 and 5: UAS ROADMAP 2005 EXECUTIVE SUMMARY
- Page 6 and 7: UAS ROADMAP 2005 TABLE OF CONTENTS
- Page 8 and 9: UAS ROADMAP 2005 FIGURE F-2: U.S. M
- Page 10 and 11: UAS ROADMAP 2005 CBP Customs and Bo
- Page 12 and 13: UAS ROADMAP 2005 ID Identification
- Page 14 and 15: UAS ROADMAP 2005 1.0 INTRODUCTION 1
- Page 16 and 17: UAS ROADMAP 2005 2.0 CURRENT UAS Th
- Page 18 and 19: UAS ROADMAP 2005 2.1.2 RQ-2B Pionee
- Page 20 and 21: UAS ROADMAP 2005 2.1.4 RQ-5A/MQ-5B
- Page 22 and 23: UAS ROADMAP 2005 2.1.6 RQ-8A/B Fire
- Page 24 and 25: UAS ROADMAP 2005 2.1.8 Joint Unmann
- Page 26 and 27: UAS ROADMAP 2005 2.1.10 I-Gnat-ER U
- Page 28 and 29: UAS ROADMAP 2005 2.1.13 Extended Ra
- Page 30 and 31: UAS ROADMAP 2005 2.2.3 Cormorant Us
- Page 34 and 35: UAS ROADMAP 2005 2.3.2 Maverick Use
- Page 36 and 37: UAS ROADMAP 2005 2.3.4 XPV-2 Mako U
- Page 38 and 39: UAS ROADMAP 2005 2.3.6 Onyx Autonom
- Page 40 and 41: UAS ROADMAP 2005 FQM-151 Pointer Ba
- Page 42 and 43: UAS ROADMAP 2005 2.4.2 Micro Air Ve
- Page 44 and 45: UAS ROADMAP 2005 launched and contr
- Page 46 and 47: UAS ROADMAP 2005 2.5.2 Tethered Aer
- Page 48 and 49: UAS ROADMAP 2005 2.5.6 High Altitud
- Page 50 and 51: UAS ROADMAP 2005 2.6 UAS PROGRAMMAT
- Page 52 and 53: UAS ROADMAP 2005 TABLE 2.7-1. CLASS
- Page 54 and 55: UAS ROADMAP 2005 3.0 REQUIREMENTS R
- Page 56 and 57: UAS ROADMAP 2005 TABLE 3.3-1. COMBA
- Page 58 and 59: UAS ROADMAP 2005 3.5 INTEROPERABILI
- Page 60 and 61: UAS ROADMAP 2005 4.0 TECHNOLOGIES U
- Page 62 and 63: UAS ROADMAP 2005 over present compu
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- Page 68 and 69: UAS ROADMAP 2005 Class A or B Misha
- Page 70 and 71: UAS ROADMAP 2005 Weight, Lb 100,000
- Page 72 and 73: UAS ROADMAP 2005 Panchromatic Calen
- Page 74 and 75: UAS ROADMAP 2005 4.4.2 Communicatio
- Page 76 and 77: UAS ROADMAP 2005 5.0 OPERATIONS 5.1
- Page 78 and 79: UAS ROADMAP 2005 labs have been inv
- Page 80 and 81: UAS ROADMAP 2005 5.3 OPERATIONS 5.3
UAS ROADMAP <strong>2005</strong><br />
2.3 SPECIAL OPERATIONS UAS<br />
2.3.1 Neptune<br />
User Service: Navy<br />
Manufacturer: DRS <strong>Unmanned</strong> Technologies<br />
Inventory: 15 Delivered/27 Planned<br />
Background: Neptune is a new tactical UA design optimized for at-sea launch and recovery. Carried in<br />
a 72x30x20 inch case that transforms into a pneumatic launcher, it can be launched from small vessels<br />
and recovered in open water. It can carry IR or color video sensors, or can be used to drop small<br />
payloads. Its digital data link is designed to minimize multipath effects over water. First flight occurred<br />
in January 2002, and an initial production contract was awarded to DRS <strong>Unmanned</strong> Technologies in<br />
March 2002.<br />
Characteristics:<br />
Neptune Neptune<br />
Length 6 ft Wing Span 7 ft<br />
Gross Weight 80 lb Payload Capacity 20 lb<br />
Fuel Capacity 18 lb Fuel Type MOGAS<br />
Engine Make 2 Stroke Power 15 hp<br />
Data Link(s) LOS C2 Frequency UHF<br />
LOS Video UHF<br />
Performance:<br />
Endurance 4 hr Max/Loiter Speeds 84/60 kt<br />
Ceiling 8,000 ft Radius 40 nm<br />
Take<strong>of</strong>f Means Pneumatic Landing Means Water/Skid/Parachute<br />
Sensor EO or IR Sensor Make DRS<br />
SECTION 2 - CURRENT UA PROGRAMS<br />
Page 20
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