Test like you Train Train like you Fight
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1 War-Winning Winning Capabilities On Time, On Cost Test like you Train Train like you Fight How Today s s Complexity Drives Future Range Requirements Major General David J. Eichhorn AFFTC Commander This Briefing is: UNCLASSIFIED 30 Oct 2008
2 The Truth
3 Overview Systems Under Test Future Systems Range Constraints Challenges Limitations Opportunities
4 CSAF s s Guidance Commitment Renew the AF s support to important mission areas Top Acquisition Priorities Expand UAV efforts Training Increase UAV pilots to 1100 by TPS Graduates will be assigned to UAVs No Modern War Has Been Won Without Air Superiority No Future War Will Be Won Without Air, Space, and Cyberspace
5 AFFTC Systems Under Test Hypersonics FAST X-51 X-37B Unmanned Aerial Systems UCAV RQ-4B MQ-9
6 X-37B Orbital Test Vehicle Cape Canaveral launch onboard a 501 version of the Atlas 5 rocket Five-meter payload fairing enclosing the spacecraft and the Centaur upper stage Re-entry and conventional landing at Vandenberg alt Edwards
7 FALCON Blackswift Global Reach Reusable Hypersonic Cruise Vehicle (HCV) Delivering 12,000 pounds of payload at a distance of 9,000 nautical miles from CONUS in less than two hours Mach 6 study Horizontal takeoff and landing 2011
8 X-51A Scramjet Engine Demonstration Mach Loaded onto a B-52 B Stratofortress Boosted by an Army Tactical Cruise Missile Release altitude 50,000 feet and will soar at hypersonic speed Pt Mugu ocean impact Mach Cruise endothermic hydrocarbon fueled Environmental assessment underway
9 Global Hawk Block 20 Certification of RQ4B Block 20 variant with EO/IR/SAR sensor suite tested at Benfield Anechoic Facility - Jun 2008 IOT&E Aug/Sep 09
10 Block 30 Global Hawk Airborne Signals Intelligence Payload (ASIP) ASIP calibration on U-2 completed at Palmdale Mar 2008 Global Hawk calibration of the ASIP sensor with the Enhanced Integrated Sensor Suite (EISS) testing underway U2 Flying Test Bed
11 Global Hawk Block 40 Multi- Platform Radar Technology Insertion Program (MP-RTIP) Operational Assessment Mojave 2008 Global Hawk air vehicle arrives 2009 Proteus Flying Test Bed
12 Predator/Reaper MQ-1 Predator Combat Hours Flown: 400,000+ Inventory: 10 Wingspan: 48.7 feet (14.8 meters) Maximum takeoff weight: 2,250 pounds Fuel Capacity: 665 pounds (100 gallons) Speed: Cruise speed around 84 mph (70 knots), up to 135 mph Range: up to 400 nautical miles (454 miles) Ceiling: up to 25,000 feet (7,620 meters) Stores 2 laser-guided AGM-114 Hellfire anti-tank MQ-9 Reaper missiles Combat Hours Flown: 4,000 + Inventory: 110 Wingspan: 66 feet (20.1 meters) Maximum takeoff weight: 10,500 pounds Payload: 3,750 pounds Speed: cruise speed around 230 miles per hour (200 knots) Range: 3,682 miles (3,200 nautical miles) Ceiling: up to 50,000 feet (15,240 meters) Stores AGM-114 Hellfire missiles GBU-12 Paveway II GBU-38 Joint Direct Attack Munitions
13 Challenges Operating Environment National Airspace System (NAS) Sense & Avoid (SAA) Controlled Airspaces Limits Available Footprint Enhanced Flight Termination System (EFTS) Space based FTS Test Readiness Environmental Assessments (EA) Failure Modes and Effects Analysis (FMEA) Risk Assessment
14 Range Constraints Today 10 Hours of Civilian Aviation Operation in the NAS 14
15 Success Hypersonic Corridors Defined EA for Corridors for X-43B X being used for test concept planning for Ground Takeoff Mach 6 Blackswift Vehicle (400 and 825 nm corridors)
16 Success Corridor for X-33 X Defined Malmstrom coverage Mountain Home coverage Dugway coverage, mid range flight Dryden/Edwards coverage
17 Flight Test to the Edge of Space Area
18 Test Readiness Environmental Assessment Impact to Air Quality Noise (mostly sonic booms) Commercial Air Traffic And more Risk Assessment Risk to uninvolved public must be acceptable Function of population, flight trajectory, vehicle size and breakup Impacts where to fly and flight test concept Public safety responsibility rests with the Range Commander
19 Test Readiness (Cont) Air Vehicle Stability & Control Flight Termination System Situation Awareness assessment data from two independent sources Failure Modes and Effects Analysis (Contractor Deliverable) Potential harm or injury to the user of the end item being designed Types System - focuses on global system functions Design - focuses on components and subsystems Process - focuses on manufacturing and assembly processes Service - focuses on service functions Software - focuses on software functions
20 Limitations Airspace Limitations Tempo of UAV and Hypersonic testing will continue to increase exponentially in the coming years FAA Partnering UAV & Hypersonic testing/deployments in the NAS under current conditions requires FAA either Temporary Flight Restriction (TFR) or Certificate of Authorization (COA) Waiver FAA has not codified standard for UAV and Hypersonic flight operating in the national airspace (NAS) platform dependant Range Infrastructure FTS EFTS & Space Based FTS immature Cognitive learning technologies need to be developed
21 Limitations (Cont) SAA, Auto Direct Surveillance Beacon (ADS-B) & TCAS Traffic Collision Avoidance System (TCAS) maturation in early development Costs to retrofit existing air vehicles with SAA/TCAS potentially significant
22 Opportunities SAA, ADS-B, & TCAS technologies Accelerate autonomous collision avoidance capabilities in both cooperative and non-cooperative air traffic needs to be developed Solution needs to be affordable and portable across multiple UAS platforms Develop robust risk assessment/containment tools to Destruct lines, glide footprint, impact prediction tools Partner with FAA for re-consideration of current operational guidance Increase number of launch and recovery sites
23
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