A Study of a Reconnaissance Surveillance Vehicle
A Study of a Reconnaissance Surveillance Vehicle A Study of a Reconnaissance Surveillance Vehicle
05.12.2012
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Engine and Control System NPS041003 84
Electrical Power Schematic NPS041003 85
- Page 33 and 34: System Overview Wide-band data tran
- Page 35 and 36: Carbon wing, tail and engine nacell
- Page 37 and 38: Design Performance NPS041003 37
- Page 39 and 40: Wing Lift Coefficient 1.40 1.20 1.0
- Page 41 and 42: Design Implementation & Design Spec
- Page 43 and 44: Navigation & Guidance Schematic NPS
- Page 45 and 46: Maintainability / Accessibility Acc
- Page 47 and 48: Integrated Sensor Suite NPS041003 4
- Page 49 and 50: Daytime IR Imagery: March 26, 1999
- Page 51 and 52: Global Hawk Airborne Integrated Com
- Page 53 and 54: Air Vehicle-to-Ground Stations Inte
- Page 55 and 56: All-Encompassing System Development
- Page 57 and 58: . Pre-flight Checkout Remove before
- Page 59 and 60: Mission Start WPt • INS alignment
- Page 61 and 62: Temperature ~ Degrees F 100 60 20 -
- Page 63 and 64: VN Diagram Global Hawk Vn Diagram L
- Page 65 and 66: Gust Exceedance (1000 Hrs) Gust Exc
- Page 67 and 68: An Example of a Flight Control HCI
- Page 69 and 70: The Air Vehicle Status HCI H367-024
- Page 71 and 72: Examples of Autonomous Operations N
- Page 73 and 74: Post-flight Checks NPS041003 73
- Page 75 and 76: Summary 1. UAVs will demonstrate lo
- Page 77 and 78: Typical Dual VMS Aircraft Loss Rate
- Page 79 and 80: Design Requirements NPS041003 79
- Page 81 and 82: Affordability UFP COTS Interchangea
- Page 83: Design Implementation & Design Spec
- Page 87 and 88: Vehicle Fuel System Schematic NPS04
- Page 89 and 90: Single Event Upsets >≅ 40 K Ft Co
- Page 91 and 92: AV2 -4 T urb ulence Even t.5 Altitu
- Page 93 and 94: Turbulence Event Conclusions � Fl
- Page 95 and 96: Typical Fault Logic, Lost Carrier N
- Page 97 and 98: Airspace Coordination Requirements
- Page 99: Civil Surveillance Requirements NPS
Electrical Power Schematic<br />
NPS041003 85