PREDATOR / REAPER SAFETY EDUCATION
Presentation for GASCo
PREDATOR / REAPER SAFETY EDUCATION Presentation for GASCo UAVs are - - PowerPoint PPT Presentation
PREDATOR / REAPER SAFETY EDUCATION Presentation for GASCo UAVs are dangerous, right? The slides in this presentation are UNCLASSIFIED These are my views and some slides may not reflect current MoD policy RAF Cat 4/5 AIR ACCIDENT RATE SINCE
Presentation for GASCo
The slides in this presentation are These are my views and some slides may not reflect current MoD policy
9 8 7 6 5 4 3 2 1
1946 48 50 52 54 56 58 60 62 64 66 68 70 72 74 76 78 80 82 84 86 88 90 92 94 96 98 00 02 08
Year Rate per 10,000 Flying hours
Reportable Accidents Fatal Accidents Accident Average
CAA CAP701
Page 38 <5700kgs non-PT GA Aircraft
Sources CAA, DASA & USAF Safety Center
SHAR 1.88/10,000fg hrs (>1979) Jag 1.02/10,000fg hrs (>1973) GR7/9 0.97/10,000fg hrs (>1988) GR1/4 0.59/10,000fg hrs (>1980) F3 0.28/10,000fg hrs (>1985) 2005 1.25/10,000fg hrs 2006 0.33/10,000fg hrs 2007 0.6/10,000fg hrs 2008 0.57/10,000fg hrs 1995 2.44/10,000fg hrs 1996 2.24/10,000fg hrs 1997 2.28/10,000fg hrs 1998 2.12/10,000fg hrs 1999 2.08/10,000fg hrs
RAF FJ Cat 4/5 AIR ACCIDENTS by Cause 1990-2000
Technical Fault 18% Human Factors (Aircrew) 39% Human Factors (Non Aircrew) 2% Not Positively Determined 14% Other 15% Natural and Operating Risk 13%
PREDATOR MISHAP by Cause 1994-2008
Technical Fault 69% Human Factors 8% Other 11% Natural and Operating Risk 11%
– Wingspan 66’ – Length 36’ – Max gross weight 10,500 lbs
– 20 hrs clean – 12+ hrs fully combat loaded
– 30K+ with weapons – 50K+ clean
500 lb bombs MQ 9 V-A10 size Hellfire
Predator Reaper
Factor GTOW 2,250 lb (1022 kg) 10,500 lb (4772 kg) 4.6 HP 105 900 8.6 Maximum Altitude 25,000 50,000+ 2 Maximum Speed 120 KTAS 250 KTAS 2 Fuel 600 lb (273 kg) 4,000 lb (1804 kg) 6.6 Payload Nose 450 lb (204 kg) 850 lb (386 kg) 1.8 Payload Wing 250 lb (113 kg) 3,000 lb (1363 kg) 12 Endurance 40 hr (18) 20+ hr (14) 0.5
MQ-1 PREDATOR A MQ-9 PREDATOR B - REAPER
Article 31 Article 32 Article 12
Flt Crew License Op Reqs “Rules of Air” Airworthiness MIL STD 516? STANAG 4671? FAR Pt23? JAR CS23??
SAFETY ENHANCEMENTS
and control surfaces
Stores Management System QUOTED SAFETY ISSUES
PREDATOR B – MQ-9 REAPER
Redundant Control Module (RCM) Processing center of flight control system Triple redundant flight computer architecture Universal Asynchronous RS RS-422 Bus (UARB) Dual redundant communication network for all flight critical nodes “Smart Smart” Servo Actuators Microcontroller based design with dual UARB interface Redundant Flight Surfaces 4 flaps, 4 ailerons, 4 ruddervators, 1 rudder Honeywell Digital Electronic Engine Control (DEEC) Engine sensor feedback (DEEC mode only) ARINC 429 interface Engine & Fuel Interface Unit (EFIU) Engine sensor feedback (DEEC and b/u mode) Dual UARB interface Triplex Embedded GPS/INS (EGI) Units Honeywell H-764 with embedded Trimble Force 5 GPS receiver Redundant data interfaces to flight computers in RCM Each EGI connected to dedicated GPS antenna Triplex Air Data Sensor Sets 3 heated pitots, 6 heated static ports 6 Precision Pressure Transducers (PPT) Alpha/Beta/OAT Probe Alpha/Beta: vanes connected to potentiometers OAT: Solid state sensor Nose Cameras with Heated Lenses 1 daylight camera, 1 long wavelength IR camera Ice Detector Magnetostrictive probe type from Goodrich Architecture 3 Flight Computer Assemblies (FCA) 2 vote processing circuits on Vote Processor Assembly 2 LOS Datalink Processor Assemblies 1 Interface Processor Assembly (IPA) Honeywell TPE331 TPE331-10YGD 10YGD-514GA turboprop engine Engine family has a long history of use in aviation applications TPE331 engines have over 100 million hours of service
PRE DAT OR B/ RE APE R
Mar itime Sur ve illanc e / Hunte r
SKY WARRIOR
U.S. Ar my Gr
r
t
PRE DAT OR
Re gional Sur ve illanc e
– 85% combat flight hours
– Direct control – In hold modes – altitude, airspeed, heading – Fully autonomous – Auto takeoff/autoland is available
– Air traffic controllers – Manned aircraft
manned aircraft long-endurance missions
PRE DAT OR C/ AVE NGE R
Ste althy? Hunte r
forest fire fighters at the national and state level
fires across nine states
Edwards AFB
time information
scarce fire fighting resources
hazards to personnel
– Patrolling the U.S. Border since October 2005 – Expanding its mission to the Northern Border, Great Lakes, both coasts and the Caribbean
Foggia - 7 Dec 04
Summit in BARI 13-14 Mar 07
– BARI pop 328,500 – CTA Class D – 45,000 Movements in 07
from 8-10 Jul 09
– L’AQUILA pop 73,000 – ROME FIR/TCA – 406,000 Movements in 08
major international civil aviation
ECAC, EASA and Eurocontrol
*Ente Nazionale per l’Aviozione Civile – Italian CAA
– 80,000 hours – 6,200 total missions
E ve r y se c ond of e ve r y day, 35+ Pr e dator
ie s air c r aft ar e air bor ne wor ldwide
– 130,000 ho urs (re pre se nts 50% g ro wth) – 10,000 to ta l missio ns
Class A-E daily
second with an accident rate comparable to MAS
damage similar to light aircraft
DE&S and ACAS
segregated airspace without Sense/Avoid
LIGHT AVIATION ASSOC PERMIT AIRCRAFT Minimum speed power off in the landing configuration not to exceed - 60 mph IAS Design dive speed not to exceed - 250 mph IAS Aircraft must be amateur built – by its owner Maximum number of seats - 2 Maximum take off weight not to exceed - 912 kgs (2006 lbs) The installed power not to exceed - 260 hp (multi engine configurations to be considered within this total installed power limit) Overflight of congested cities/towns recently approved by CAA until Jul 10…
– JSPs 550 and 553 – JAP 100A – Def Stans 00-970, 05-57, 05-122, 05-123, 05-130
Nose Cameras with Heated Lenses 1 daylight camera, 1 long wavelength IR camera
Ground Control Station
IR Picture >10nm Day EO Picture >10nm Taken at 10,000ft by a US REAPER