USAF Strike Fighters. An analysis of range, stamina, turning, and acceleration

Similar documents
USAF Strike Fighters. An analysis of range, stamina, turning, and acceleration By Spurts

Compared Air Combat Performances analysis Mig-21 versus F-5E

Table of Contents Aircraft... 4

Compared Air Combat Performances analysis Mig-21 versus F-4 Phantom II Part 1

WHEN BORDER SECURITY MATTERS

Appenidix E: Freewing MAE UAV analysis

AE 451 Aeronautical Engineering Design Final Examination. Instructor: Prof. Dr. Serkan ÖZGEN Date:

In this lecture... Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay

Basic hypothesis. Subjective position may give less Drag at high Mach number to the Typhoon and better Lift at high AoA (>20) for the Rafale.

RDT&E BUDGET ITEM JUSTIFICATION SHEET (R-2 Exhibit) February 2003

Classical Aircraft Sizing I

Design Considerations for Stability: Civil Aircraft

Mike Gibbons Paul Summers John Murnane

Visit Beechcraft.com or contact a defense company sales rep:

General Dynamics F-16 Fighting Falcon

WHY TWO SPOOLS ARE BETTER THAN ONE: EQUIPPING OUR MILITARY WITH THE BEST TECHNOLOGY FOR EXISTING AND EMERGING THREATS

Performance means how fast will it go? How fast will it climb? How quickly it will take-off and land? How far it will go?

AVIATION OPERATIONAL MEASURES FOR FUEL AND EMISSIONS REDUCTION WORKSHOP Weight Management

How to use the Multirotor Motor Performance Data Charts

F-5E Tiger II USER MANUAL. Virtavia F-5E Tiger II DTG Steam Edition Manual Version 2.0

High aspect ratio for high endurance. Mechanical simplicity. Low empty weight. STOVL or STOL capability. And for the propulsion system:

Overview of WWII Part 1

GRWW1 5b Zeppelin airships

Mc Donnell Douglas F-4E Blk.41 Phantom II (J79-GE-17)

BAYLOR UNIVERSITY DEPARTMENT OF ENGINEERING. EGR 4347 Analysis and Design of Propulsion Systems Fall 2002 ASSIGNMENT GUIDELINES

North American F-86F Sabre USER MANUAL. Virtavia F-86F Sabre DTG Steam Edition Manual Version 1

Team 2. AAE451 System Requirements Review. Chad Carmack Aaron Martin Ryan Mayer Jake Schaefer Abhi Murty Shane Mooney

Environmentally Focused Aircraft: Regional Aircraft Study

Analysis of JSF Prototypes

Flight Test Evaluation of C-130H Aircraft Performance with NP2000 Propellers

Preface. Acknowledgments. List of Tables. Nomenclature: organizations. Nomenclature: acronyms. Nomenclature: main symbols. Nomenclature: Greek symbols

CONCEPTUAL DESIGN OF UTM 4-SEATER HELICOPTER. Mohd Shariff Ammoo 1 Mohd Idham Mohd Nayan 1 Mohd Nasir Hussain 2

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited.

When. The power and precision of USAF s F-15E Strike Eagles starts with the Fourth Fighter Wing.

PERFORMANCE ANALYSIS OF UNMANNED AIR VEHICLE INTERCEPTOR (UAV-Ip)

AE 451 Aeronautical Engineering Design I Estimation of Critical Performance Parameters. Prof. Dr. Serkan Özgen Dept. Aerospace Engineering Fall 2015

A-6E Intruder USER MANUAL. Virtavia A-6E Intruder DTG Steam Edition Manual Version 2.0

AN ADVANCED COUNTER-ROTATING DISK WING AIRCRAFT CONCEPT Program Update. Presented to NIAC By Carl Grant November 9th, 1999

Weaponizing Small Unmanned Aircraft Systems. Cody Tretschok Capture Manager, Advanced UAS Weapons Advanced Missiles and Unmanned Systems

Beechcraft Bonanza. 550 Tuned Induction Conversion. STC for Teledyne Continental IO-550-R for the Beechcraft Bonanza

Aeronautical Systems Center

Aeronautical Engineering Design II Sizing Matrix and Carpet Plots. Prof. Dr. Serkan Özgen Dept. Aerospace Engineering Spring 2014

Rotary Wing Micro Air Vehicle Endurance

2017 FINANCIAL ANALYSIS

64MM F-16 Fighting Falcon V2

Flying Low and Slow. (and the Tools for its Calculation) Dieter Scholz. Hamburg University of Applied Sciences

AIAA Foundation Undergraduate Team Aircraft Design Competition. RFP: Cruise Missile Carrier

Economic Impact of Derated Climb on Large Commercial Engines

Versatile Affordable Advanced Turbine Engines Provide Game Changing Capability with Superior Fuel Efficiency

RDT&E BUDGET ITEM JUSTIFICATION SHEET (R-2 Exhibit) February 2003

ELECTRIC POWER TRAINS THE KEY ENABLER FOR CONTRA ROTATING PROPELLERS IN GENERAL AVIATION (& VICE VERSA)

OPTIMAL MISSION ANALYSIS ACCOUNTING FOR ENGINE AGING AND EMISSIONS

Fire Fighting Equipment Development - Unmanned Aerial Vehicle Trials. Ripley Valley Rural Fire Brigade - August 2010

Mc Donnell Douglas F-4D Blk.37 Phantom II (J79-GE-15)

blended wing body aircraft for the

Virginia Tech DD-21 Destroyer Concept. David Woodward Ben Spina Jon Law Steve Darsie Andrew Girdler Jessica Smoldt

DESIGN AND PERFORMANCE ANALYSIS OF SINGLE INLET MULTIPLE OUTLET JET NOZZLE WITH THRUST VECTOR CONTROL

Advanced Propulsion Concepts for the HYDRA-70 Rocket System

Span m [65.16 ft] Length m [43.89 ft] Height m [12.08 ft]

Single or Twin Motors?

A Space Solar Power Industry for $2 Billion or Your Money Back

INDEX. Preflight Inspection Pages 2-4. Start Up.. Page 5. Take Off. Page 6. Approach to Landing. Pages 7-8. Emergency Procedures..

Electric VTOL Aircraft

LIQUID HYDROGEN AS AVIATION FUEL AND ITS RELATIVE PERFORMANCE WITH COMMERCIAL AIRCRAFTS FUEL

Future Vision in Composites & Manufacturing and their Challenges. Lars Sjostrom Director Future Business Saab Aeronautics

1. Ship Name. 5. Type 6. Size Class/ Description. Damage Points. Surface Speed. Submerged Speed. Embarked Aircraft

User Guide. Vought F2G "Super" Corsair. ... print your plane www. 3DPrintedKits.com. Scale ~ 1:6.6 Wingspan 1.9m/75in

Multidisciplinary Design Optimization of a Truss-Braced Wing Aircraft with Tip-Mounted Engines

Cost Benefit Analysis of Faster Transmission System Protection Systems

Eurofighter -Typhoon Entwicklungsprogramm. Peter Huber Chief Engineer Typhoon CASSIDIAN AS

A Cost Benefit Analysis of Faster Transmission System Protection Schemes and Ground Grid Design

Military, Aerospace, and Manufacturing Test Solutions

Predator B: The Multi-Role UAV

JIM BEDE ADDS TWO HOMEBUILTS TO HIS LINE - THE BD-5J AND THE ALL NEW BD-6

Three major types of airplane designs are 1. Conceptual design 2. Preliminary design 3. Detailed design

Welcome to the Airbus A380 Basic Manual for Virtual Air Cadet Airlines.

Classical Aircraft Sizing II

Versatile Affordable Advance Turbine Engine (VAATE)

Exhibit R-2, RDT&E Budget Item Justification

Weight Effects Part 1

ADVENT. Aim : To Develop advanced numerical tools and apply them to optimisation problems in engineering. L. F. Gonzalez. University of Sydney

PROJECT HAVE DOUGHNUT -

In order to discuss powerplants in any depth, it is essential to understand the concepts of POWER and TORQUE.

Aermacchi M-345 THE NEXT GENERATION TRAINER

«DO160/ED14» - Jessica France

EW Engagement Modelling for Light Armoured Vehicles

AIRCRAFT CONCEPTUAL DESIGN USING MULTI- OBJECTIVE OPTIMISATION.

Mathematics of Flight. Distance, Rate and Time

DESIGNING AND DEVELOPMENT OF UNMANNED AERIAL VEHICLE

The Airplane That Could!

DUCHESS BE-76 AND COMMERCIAL MULTI ADD-ON ORAL REVIEW FOR CHECKRIDE

neuron An efficient European cooperation scheme

AIRPLANE PERFORMANCES

AIRCRAFT DESIGN SUBSONIC JET TRANSPORT

Airframes Instructor Training Manual. Chapter 6 UNDERCARRIAGE

PRODUCT CODE Av3 FLIGHT PLANNING EXAM 2 WORKING. by Rob Avery

Multidisciplinary Design Optimization of a Strut-Braced Wing Transonic Transport

POWER. SAFETY. PERFORMANCE. ALL IN ONE PACKAGE.

North American XB-70A Valkyrie USER MANUAL. Virtavia XB-70A Valkyrie DTG Steam Edition Manual Version 1

Running head: GYROSCOPIC STABILIZATION VS. STABILIZATION FINS 1

Transcription:

USAF Strike Fighters An analysis of range, stamina, turning, and acceleration

The Contenders There are currently slated to be three USAF strike aircraft in the 2020 timeframe F-15E Strike Eagle One of the largest and heaviest fighter aircraft Massive fuel/weapons capacity F-16C Fighting Falcon One of the smallest and lightest fighter aircraft Diminutive fuel capacity, but retains over half the weapons capacity of the F-15E F-35A Lightning II External dimensions similar to F-16, but weight similar to F-15C Tremendous internal fuel/weapon capacity for it s size Will also look at F-16C with conformal fuel tanks (referenced as F-16I)

Specs F-15E Empty Weight: 38,700 lbs Box volume (LxWxH): 50,517 cubic feet Fuel A2A A2G Internal: 22,300 lbs External: 12,000 lbs 3 600gallon tanks on heavy A2G stations AIM-120 up to 8 One each on four conformal heavy stations One each on four dedicated AAM stations AIM-9 up to 4 One each on four dedicated AAM stations Up to 7 heavy stations One under each wing One on centerline Four conformal to the lower fuselage Targeting Pods - External F-16C (I) Empty Weight: 20,300 lbs (22,300 lbs) Box volume (LxWxH): 25,898 cubic feet Fuel A2A A2G Internal: 7,000 lbs (10,200 lbs) External: 7,000 lbs 2 370gallon tanks on heavy A2G stations 1 300gallon tank on centerline station AIM-120 up to 6 One each on two heavy stations One each on four dedicated AAM stations AIM-9 up to 6 One each on two heavy stations One each on four dedicated AAM stations Up to 4 heavy stations Targeting Pods External

Specs F-35A Empty Weight: 29,400 lbs Box volume (LxWxH): 25,546 cubic feet Fuel A2A Internal: 18,200 lbs External: 5,800 lbs 2 426gallon tanks on heavy A2G stations AIM-120 up to 14 Internal 6 Two each per heavy station One each on dedicated AAM station External 8 AIM-9 up to 10 two each per heavy station Two each per external heavy station One each on dedicated AAM station A2G Up to 6 heavy stations Two internal Four external Targeting Pods - internal

Specs conclusion The considerable empty weight of the dimensionally small F-35 is accounted for by it s internal carriage of large fuel volumes, two heavy A2G stations, two A2A stations, and Targeting equipment Despite the F-35 only having 4 dedicated AAM stations, the ability to carry two missiles per heavy station gives it vast flexibility

Missions 500nm Endurance If tanks are carried then they are assumed to be carried throughout mission Assumed time/performance critical target appears as soon as aircraft is on station (most fuel remaining, worst performance) Tanks are dropped Instant/Sustained turn taken at cruise speed.8m to 1.2M acceleration measured Additional factors Max Range calculated as alternate mission plan Two flight profiles calculated Optimum max range profile Mission dictated 20,000ft at 0.8M

Drag drag areas estimated from Max Endurance F-15E Base Drag Area: 21.71 Mission based AA 23.33 AA with tanks 25.00 AG 24.54 AG with tanks 26.52 F-16C (I) Base Drag Area: 9.07 (9.21) Mission based AA 10.57 (10.71) AA with tanks 12.94 (13.08) AG 13.30 (13.44) AG with tanks 16.42 (16.56)

Drag F-35 Base Drag Area: 9.75 Mission based AA 9.75 AA with tanks 12.42 AG 9.75 AG with tanks 12.42

Drag conclusion Despite the natural low drag of the F-16 airframe the addition of missiles, bombs, pylons, tanks, and targeting pods nearly doubles it s base drag. The low drag of the F-35 will allow for higher cruise speeds and/or greater range, the two being a natural tradeoff. The drag areas of the clean F-16 and F-35 are consistent with the story of an F-35 with 9 tons of internal fuel/weapons (traditional T/W of.59) out climbing the F-16 chase plane that was carrying only a centerline gas tank (traditional T/W of.61) while in military power.

500nm CAP Altitude with Distance All aircraft are able to top off at the tanker right at their optimum altitudes. 40 39 38 Cruise Speeds: F-16C/CFT (EFT) -.84/.84 (.83/.82) F-15E (EFT) -.87(.85) F-35A (CFT) -.87(.85) The added weight of extra fuel (CFT and/or EFT has a huge impact on best cruise altitude F-35A with EFT has same cruise altitudes as F-16C with CFT 37 36 35 34 33 32 31 F-15E F-16C F-16C(CFT) F-35A F-15E EFT F-16C EFT F-16C (CFT) EFT F-35A EFT For non-optimum cruise all aircraft are traveling at 0.8M at 20,000ft. 30 29 28 0 100 200 300 400 500

500nm CAP Endurance F-35A opt Optimum cruise data assumes constant climb as fuel is burned and all missiles are retained. F-16I opt F-16C opt EFTs are retained for entire mission Under Optimum Cruise, the F-35 can loiter longer while clean than even a Strike Eagle. Under a constrained flight plan most of the aircraft have around 30 minutes of clean endurance. The F-16C cannot make a 500nm cruise at 20kft without drop tanks F-15E opt F-35A 20k F-16I 20k Clean EFTs The two 426 gallon drop tanks on the F-35A provide such a small increase in fuel fraction but increase drag by about 27% The F-35 is the only aircraft that is out of fuel in the external tanks before reaching 500nm. F-16C 20k F-15E 20k

Dogfight 500nm out Aircraft get bounced as soon as they are on station, the most fuel on board gives the worst performance. Any EFTs are dropped. The F-16 has very high placard limits under air to air loading and is drag limited Speed F-35A opt F-16I opt F-16C opt F-15E opt The F-15E and F-35 have more thrust than their placard limits allow The F-35s placard limit is often above the placard/thrust limits of it s brethren, only A-A configured F-16 are faster. F-35A 20k F-16I 20k AB Redline Mil F-16C 20k F-15E 20k

Dogfight 500nm out Aircraft get bounced as soon as they are on station, the most fuel on board gives the worst performance. Any EFTs are dropped. Cruise-1.2M acceleration F-35A opt F-16I opt In Optimum Cruise scenarios the added weight of the extra fuel in the dropped EFT group is mitigated by the lower altitude. F-16C opt F-15E opt Dropped EFTs 0.8-1.2M acceleration, while one of the standard JSF parameters, is rather arbitrary if flown at Optimum Cruise as it starts out between.84 and.87 depending on aircraft F-35A 20k F-16I 20k Clean F-16C 20k F-15E 20k

Dogfight 500nm out Turn rate at cruise speed (clean above dropped EFTs) Aircraft get bounced as soon as they are on station, the most fuel on board gives the worst performance. Any EFTs are dropped. In Optimum Cruise scenarios the added weight of the extra fuel in the dropped EFT group is mitigated by the lower altitude. 20.0 18.0 16.0 14.0 12.0 10.0 8.0 6.0 4.0 2.0 0.0 Instant Turn Sustained Turn All aircraft are lift limited in these scenarios with the exception of the F-35 at 20kfeet and 0.8M in which it is right at corner velocity. Data found coincides with statements of Sustained Turns similar to F-16 with Instantaneous Turns similar to F/A-18. While lift limited the F-35 can out point the F-16 at the expense of energy. This is a true apples-apples mission based performance, not 50% fuel with two AIM-120s 20.0 18.0 16.0 14.0 12.0 10.0 8.0 6.0 4.0 2.0 0.0 Instant Turn Sustained Turn

Osirak style escort mission Max Range EFTs are dropped as soon as they are empty The Constrained Flight Plan at 20,000ft shows results similar to the number compared to the KPP, but we can see that no clean strike aircraft is going to significantly exceed that range. F-35A opt F-16I opt F-16C opt F-15E opt While the F-16 is a hotrod in acceleration, it suffers greatly in range compared to the heavier aircraft F-35A 20k Clean EFTs F-16I 20k F-16C 20k F-15E 20k

500nm Interdiction Altitude with Distance All aircraft are able to top off at the tanker right at their optimum altitudes. Cruise Speeds: F-16C/CFT (EFT) -.83/.81 (.80/.80) F-15E (EFT) -.86(.83) F-35A (CFT) -.87(.85) The added weight of extra fuel (CFT and/or EFT has a huge impact on best cruise altitude The added weight of targeting pods as well as the drag of the targeting pods and bombs (and interference drag between bombs and tanks) robs the 4 th Gen aircraft of their performance 37 36 35 34 33 32 31 30 29 28 F-15E F-16C F-16C(CFT) F-35A F-15E EFT F-16C EFT F-16C (CFT) EFT F-35A EFT For non-optimum cruise all aircraft are traveling at 0.8M at 20,000ft. 27 26 0 100 200 300 400 500

500nm Interdiction Endurance F-35A opt Optimum cruise data assumes constant climb as fuel is burned and all missiles are retained. F-16I opt F-16C opt EFTs are retained for entire mission Under Optimum Cruise, the F-35 can loiter longer while clean than even a Strike Eagle. The F-16C cannot make a 500nm cruise at any altitude without drop tanks, adding CFTs still requires an Optimum Cruise. F-15E opt F-35A 20k F-16I 20k Clean EFTs The two 426 gallon drop tanks on the F-35A provide such a small increase in fuel fraction but increase drag by about 27% The F-35 is the only aircraft that is out of fuel in the external tanks before reaching 500nm. F-16C 20k F-15E 20k

Dogfight 500nm out Aircraft get bounced as soon as they are on station, the most fuel on board gives the worst performance. Any EFTs are dropped. Both placard and drag limit speeds are reduced drastically for the F-16 The F-15E and F-35 have more thrust than their placard limits allow The F-35s is unquestionably the fastest strike aircraft of the group. Speed F-35A opt F-16I opt F-16C opt F-15E opt F-35A 20k AB Redline F-16I 20k F-16C 20k Mil F-15E 20k

Dogfight 500nm out Aircraft get bounced as soon as they are on station, the most fuel on board gives the worst performance. Any EFTs are dropped. Cruise-1.2M acceleration F-35A opt F-16I opt In Optimum Cruise scenarios the added weight of the extra fuel in the dropped EFT group is mitigated by the lower altitude. F-16C opt F-15E opt Dropped EFTs 0.8-1.2M acceleration, while one of the standard JSF parameters, is rather arbitrary if flown at Optimum Cruise as it starts out between.80 and.87 depending on aircraft F-16 with CFT cannot reach 1.2M at 20kft, time listed is to reach 1.17M Compared to A-A loadouts, the F-35 goes from competitive to the hotrod of the group while the previous hotrod is pushing it s drag limits F-35A 20k F-16I 20k F-16C 20k F-15E 20k Clean

Dogfight 500nm out Turn rate at cruise speed (clean above dropped EFTs) Aircraft get bounced as soon as they are on station, the most fuel on board gives the worst performance. Any EFTs are dropped. In Optimum Cruise scenarios the added weight of the extra fuel in the dropped EFT group is mitigated by the lower altitude. 20.0 18.0 16.0 14.0 12.0 10.0 8.0 6.0 4.0 2.0 0.0 Instant Turn Sustained Turn All aircraft are lift limited in these scenarios with the exception of the F-35 at 20kfeet and 0.8M in which it is right at corner velocity. 20.0 18.0 16.0 14.0 12.0 10.0 8.0 6.0 4.0 2.0 0.0 Instant Turn Sustained Turn

Osirak style strike mission Max Range EFTs are dropped as soon as they are empty The Constrained Flight Plan at 20,000ft shows results similar to the number compared to the KPP, but we can see that no clean strike aircraft is going to significantly exceed that range. F-35A opt F-16I opt F-16C opt F-15E opt In the Strike role, the F-35 clean has range similar to F-16s with EFTs (sometimes greater still) and comparable to the significantly larger Strike Eagle F-35A 20k F-16I 20k Clean EFTs F-16C 20k F-15E 20k

Conclusions We see that under actual combat conditions the F-35 can climb, run, and turn as well as or better than it s stable mates. It does this while having a better ECM/EA suite, full IR targeting and spherical tracking, secure LPI networking, and all aspect X-Band VLO. In short it is more capable than anything that has ever been used in combat before Optimum Profile was done to show how Max Range mission data could be gathered as these represent leaving a tanker and returning to a tanker with reserves based on aircraft weight, a true best case scenario. Constrained Profile was done to show how mission planners and battlespace managers may not want aircraft going across so many altitudes, and max range at 20kft was at much lower speeds than the 0.8M calculated but the mission planners also can t afford to simply wait around When looking at the F-35s clean range at altitudes above 30kft it is easy to see how the last 75nm in and out could be done as 1.25M and still make a 500nm+ range, which falls in line with the statement 150nm of cruise at 1.25M. I may do a case study on this in the future.