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LOS Datalink SAR MTI EO IR
Wide Area Search Target Coverage Location Accuracy
12,000 NMI 65,000 Ft* (66,400 Ft Demonstrated) 36 Hrs* (31.5 Hrs Demonstrated) 1 Loss in 605 1.5, 8.67*, 20*, 30*, 40*, 47.9* Mbps 137* Mbps 1.0/0.3m resolution (WAS/Spot)* 20 - 200Km/10m Range resolution* EO NIIRS 6.5/6.0 (Spot/WAS) IR NIIRS 5.5/5.0 (Spot/WAS)* 40,000 Sq. NMI/Day 1,900 Spots Targets /Day < 20 meter CEP*
Increase the Reach of Existing and Future Surveillance Systems
Extraordinary Range and Endurance
Fewer Number of Systems Required to Maintain Global ISR Coverage
Maximum Speed:
410 kts. TAS
Operational Ceiling: over 70,000 feet
Max Unrefueled Range: over 3,000 NM
Length:
97 feet
Wingspan:
94 feet
Max Takeoff Wt:
130,000 lb.
Global Hawk Flight Critical Systems Feature Dual Redundancy
- Cross Channel Data Link
Inboard Ailerons
Outboard Spoilers
Outboard Ruddervators
Dual FADECs* Dual Air Data Systems Dual Dissimilar Navigation Systems
Standard Runway 8,000’ x 150’
Global Hawk Vehicle Size
U-2
B-737
Global Hawk
Length:
63.1 feet
Wingspan:
104.8 feet
Height:
16.7 feet (at tail)
Max Takeoff Wt:
40,000 lb.
Altitude
Endurance (hours)
2 ApproAvepdprfoovrePdufbolricPRuebleicaRseelease 00/00/00 February 20, 2002
Speed (n.miles/hour)
Global Hawk Is an Integrated System
USAF Acquisition Schedule
(for DAB)
Milestones
FY00
FY01
FY02
FY03
FY04
FY05
MS II/LRIP IOT&E MS III
FY06
FY07
FY08
FY09
Program Schedule
Block 5/ Spiral 1 Dev
Approved for Public Release Document Number: ASC 02-0340 February 20, 2002
Air Combat Systems Unmanned Systems
Why Global Hawk?
Provide Continuous Day/Night, High Altitude, All Weather Surveillance Reconnaissance in Direct Support of Allied Ground and Air Forces Across the Spectrum of Conflict
Inboard Ruddervators
Dual IMMCs* Dual Flight Critical Buses Dual Power Buses
IMMC- Integrated Mission Management Computer
Global Hawk
Performance Summary
CHARACTERISTICS
ACTD DEMONSTRATED and PROJECTED PERFORMANCE
Maximum Range Maximum Altitude Maximum Endurance Flight Critical Reliability SATCOM Datalink
C2 LOS ATC VOICE
LAUNCH AND
RECOVERY ELEMENT (C2 ONLY)
Global Hawk HAE UAV
Notional Mission Profile
6 ApproAvepdprfoovrePdufbolricPRuebleicaRseelease 00/00/00 February 20, 2002
Loiter Speed:
573 kts. TAS
Operational Ceiling: 40,000 feet
Max Unrefueled Range: 2,700 NM
7 ApproAvepdprfoovrePdufbolricPRuebleicaRseelease 00/00/00 February 20, 2002
• 20-200 Km Range • ±45° Azimuth
(Either Side of Aircraft)
GMTI 4 Kts Detectable 6 Range Bars 10 M Range Resolution
11 ApproAvepdprfoovrePdufbolricPRuebleicaRseelease 00/00/00 February 20, 2002
ATC Voice
Ku SATCOM
UHFSATCOM
C2 & SENSOR
C2 & SENSOR
C2
C2
C2
MISSION CONTROL
ELEMENT (C2 &
SENSOR)
CDL C2 & SENSOR
SENSOR
CDL SENSOR
TACTICAL USERS (SENSOR ONLY)
5 ApproAvepdprfoovrePdufbolricPRuebleicaRseelease 00/00/00 February 20, 2002
来自百度文库
PROGRAM GOALS
14,000 NMI 65,000 FT+ 42 Hrs 1 Loss in 200 Missions 1.5 - 50 Mbps > 50 Mbps 1.0/0.3m resolution (WAS/Spot) 20 - 200Km/10m Range resolution EO NIIRS 6.5/6.0 (Spot/WAS) IR NIIRS 5.5/5.0 (Spot/WAS) 40,000 Sq. NMI/Day 1,900 Spots Targets /Day < 20 meter CEP
RQ-4A Global Hawk
High Altitude Endurance Unmanned Aerial Reconnaissance System
USAF System Program Office
Aeronautical Systems Center ISR Programs (ASC/RAV)
• WAS: 40,000 sq. nmi/day • Spot: 1900 (2 km x 2 km) spots/day • Geolocation Accuracy: 20 m CEP • All Digital Servo • 3 mrad Stabilization • Internal Environmental Control • Detector/Dewar based on HAC Staring
Global Hawk System Overview
IN M A R S AT C 2
COMMUNICATIONS
UHF-Band: C2 LOS C2 SATCOM
IN M A R S AT o r E q u iv alen t
Ku-Band: C2 and Sensor SATCOM
X-Band CDL: C2 and Sensor LOS
3 ApproAvepdprfoovrePdufbolricPRuebleicaRseelease 00/00/00 February 20, 2002
Global Hawk Industrial Base Team
Air Segment
4 ApproAvepdprfoovrePdufbolricPRuebleicaRseelease 00/00/00 February 20, 2002
Campaign • EO Detector COTS Based
Global Hawk Airborne Integrated Communications Subsystem
13 ApproAvepdprfoovrePdufbolricPRuebleicaRseelease 00/00/00 February 20, 2002
9 ApproAvepdprfoovrePdufbolricPRuebleicaRseelease 00/00/00 February 20, 2002
* Demonstrated Performance
Global Hawk Integrated Sensor Suite
10 ApproAvepdprfoovrePdufbolricPRuebleicaRseelease 00/00/00 February 20, 2002
Strip 10 Km Swath 1 M Resolution
Global Hawk
EO/IR Sensor Summary Data
Physical Parameters • Weight: 220 lbs • Volume: 15.6 CF • Power: 582 W (28 Vdc)
12 ApproAvepdprfoovrePdufbolricPRuebleicaRseelease 00/00/00 February 20, 2002
Length:
44.4 feet
Wingspan:
116 feet
Height:
15.2 feet (at tail)
Max.Takeoff Wt:
25,600 lb.
Loiter Speed:
343 kts. TAS
Operational Ceiling: 65,000 feet
Max Unrefueled Range:over 12,000 NM
Global Hawk
SAR/MTI Sensor Summary Data
Spot 2 Km x 2 Km 0.3 M Resolution
Radar Characteristics
• X-Band Frequency
• 3 Radar Modes on Land
• New Maritime Modes for Australian Deployment
FADEC - Full Authority Digital Engine Control
8 ApproAvepdprfoovrePdufbolricPRuebleicaRseelease 00/00/00 February 20, 2002
Inboard Spoilers
Outboard Ailerons
Features
• Dual Spectral Bands – Visible: 0.4 – 0.8 mm – MWIR: 3.6 – 5.0 mm
• NIIRS – Visible: 6.5 @ 45° Roll (28 km) – MWIR: 5.5 @ 45° Roll (28 km)
• FOR: ±80° Roll ±15° Pitch
Wide Area Search Target Coverage Location Accuracy
12,000 NMI 65,000 Ft* (66,400 Ft Demonstrated) 36 Hrs* (31.5 Hrs Demonstrated) 1 Loss in 605 1.5, 8.67*, 20*, 30*, 40*, 47.9* Mbps 137* Mbps 1.0/0.3m resolution (WAS/Spot)* 20 - 200Km/10m Range resolution* EO NIIRS 6.5/6.0 (Spot/WAS) IR NIIRS 5.5/5.0 (Spot/WAS)* 40,000 Sq. NMI/Day 1,900 Spots Targets /Day < 20 meter CEP*
Increase the Reach of Existing and Future Surveillance Systems
Extraordinary Range and Endurance
Fewer Number of Systems Required to Maintain Global ISR Coverage
Maximum Speed:
410 kts. TAS
Operational Ceiling: over 70,000 feet
Max Unrefueled Range: over 3,000 NM
Length:
97 feet
Wingspan:
94 feet
Max Takeoff Wt:
130,000 lb.
Global Hawk Flight Critical Systems Feature Dual Redundancy
- Cross Channel Data Link
Inboard Ailerons
Outboard Spoilers
Outboard Ruddervators
Dual FADECs* Dual Air Data Systems Dual Dissimilar Navigation Systems
Standard Runway 8,000’ x 150’
Global Hawk Vehicle Size
U-2
B-737
Global Hawk
Length:
63.1 feet
Wingspan:
104.8 feet
Height:
16.7 feet (at tail)
Max Takeoff Wt:
40,000 lb.
Altitude
Endurance (hours)
2 ApproAvepdprfoovrePdufbolricPRuebleicaRseelease 00/00/00 February 20, 2002
Speed (n.miles/hour)
Global Hawk Is an Integrated System
USAF Acquisition Schedule
(for DAB)
Milestones
FY00
FY01
FY02
FY03
FY04
FY05
MS II/LRIP IOT&E MS III
FY06
FY07
FY08
FY09
Program Schedule
Block 5/ Spiral 1 Dev
Approved for Public Release Document Number: ASC 02-0340 February 20, 2002
Air Combat Systems Unmanned Systems
Why Global Hawk?
Provide Continuous Day/Night, High Altitude, All Weather Surveillance Reconnaissance in Direct Support of Allied Ground and Air Forces Across the Spectrum of Conflict
Inboard Ruddervators
Dual IMMCs* Dual Flight Critical Buses Dual Power Buses
IMMC- Integrated Mission Management Computer
Global Hawk
Performance Summary
CHARACTERISTICS
ACTD DEMONSTRATED and PROJECTED PERFORMANCE
Maximum Range Maximum Altitude Maximum Endurance Flight Critical Reliability SATCOM Datalink
C2 LOS ATC VOICE
LAUNCH AND
RECOVERY ELEMENT (C2 ONLY)
Global Hawk HAE UAV
Notional Mission Profile
6 ApproAvepdprfoovrePdufbolricPRuebleicaRseelease 00/00/00 February 20, 2002
Loiter Speed:
573 kts. TAS
Operational Ceiling: 40,000 feet
Max Unrefueled Range: 2,700 NM
7 ApproAvepdprfoovrePdufbolricPRuebleicaRseelease 00/00/00 February 20, 2002
• 20-200 Km Range • ±45° Azimuth
(Either Side of Aircraft)
GMTI 4 Kts Detectable 6 Range Bars 10 M Range Resolution
11 ApproAvepdprfoovrePdufbolricPRuebleicaRseelease 00/00/00 February 20, 2002
ATC Voice
Ku SATCOM
UHFSATCOM
C2 & SENSOR
C2 & SENSOR
C2
C2
C2
MISSION CONTROL
ELEMENT (C2 &
SENSOR)
CDL C2 & SENSOR
SENSOR
CDL SENSOR
TACTICAL USERS (SENSOR ONLY)
5 ApproAvepdprfoovrePdufbolricPRuebleicaRseelease 00/00/00 February 20, 2002
来自百度文库
PROGRAM GOALS
14,000 NMI 65,000 FT+ 42 Hrs 1 Loss in 200 Missions 1.5 - 50 Mbps > 50 Mbps 1.0/0.3m resolution (WAS/Spot) 20 - 200Km/10m Range resolution EO NIIRS 6.5/6.0 (Spot/WAS) IR NIIRS 5.5/5.0 (Spot/WAS) 40,000 Sq. NMI/Day 1,900 Spots Targets /Day < 20 meter CEP
RQ-4A Global Hawk
High Altitude Endurance Unmanned Aerial Reconnaissance System
USAF System Program Office
Aeronautical Systems Center ISR Programs (ASC/RAV)
• WAS: 40,000 sq. nmi/day • Spot: 1900 (2 km x 2 km) spots/day • Geolocation Accuracy: 20 m CEP • All Digital Servo • 3 mrad Stabilization • Internal Environmental Control • Detector/Dewar based on HAC Staring
Global Hawk System Overview
IN M A R S AT C 2
COMMUNICATIONS
UHF-Band: C2 LOS C2 SATCOM
IN M A R S AT o r E q u iv alen t
Ku-Band: C2 and Sensor SATCOM
X-Band CDL: C2 and Sensor LOS
3 ApproAvepdprfoovrePdufbolricPRuebleicaRseelease 00/00/00 February 20, 2002
Global Hawk Industrial Base Team
Air Segment
4 ApproAvepdprfoovrePdufbolricPRuebleicaRseelease 00/00/00 February 20, 2002
Campaign • EO Detector COTS Based
Global Hawk Airborne Integrated Communications Subsystem
13 ApproAvepdprfoovrePdufbolricPRuebleicaRseelease 00/00/00 February 20, 2002
9 ApproAvepdprfoovrePdufbolricPRuebleicaRseelease 00/00/00 February 20, 2002
* Demonstrated Performance
Global Hawk Integrated Sensor Suite
10 ApproAvepdprfoovrePdufbolricPRuebleicaRseelease 00/00/00 February 20, 2002
Strip 10 Km Swath 1 M Resolution
Global Hawk
EO/IR Sensor Summary Data
Physical Parameters • Weight: 220 lbs • Volume: 15.6 CF • Power: 582 W (28 Vdc)
12 ApproAvepdprfoovrePdufbolricPRuebleicaRseelease 00/00/00 February 20, 2002
Length:
44.4 feet
Wingspan:
116 feet
Height:
15.2 feet (at tail)
Max.Takeoff Wt:
25,600 lb.
Loiter Speed:
343 kts. TAS
Operational Ceiling: 65,000 feet
Max Unrefueled Range:over 12,000 NM
Global Hawk
SAR/MTI Sensor Summary Data
Spot 2 Km x 2 Km 0.3 M Resolution
Radar Characteristics
• X-Band Frequency
• 3 Radar Modes on Land
• New Maritime Modes for Australian Deployment
FADEC - Full Authority Digital Engine Control
8 ApproAvepdprfoovrePdufbolricPRuebleicaRseelease 00/00/00 February 20, 2002
Inboard Spoilers
Outboard Ailerons
Features
• Dual Spectral Bands – Visible: 0.4 – 0.8 mm – MWIR: 3.6 – 5.0 mm
• NIIRS – Visible: 6.5 @ 45° Roll (28 km) – MWIR: 5.5 @ 45° Roll (28 km)
• FOR: ±80° Roll ±15° Pitch