A1-Mc Donnell Douglas F-4D Blk.37-NFM--r1 PERFORMANCE ANALYSIS Mc Donnell Douglas F-4D Blk.37 Phantom II (J79-GE-15) CAUTION STATEMENT : This document is to be use only for simulation. Do not try to apply the procedures and or advices contained in it if you have the opportunity to fly this plane in real life. By the way, if you had (or still have) flew this aircraft, your comments, criticism and more are welcome LICENSE : This document has been created by J.M. LANGERON / TOPOLO, (http://topolo.free.fr/) all the values used to model the aircraft behavior have been computed by him, like all performance charts presented here. If you want to use these data, or part of it, please contact the author by personal message to TOPOLO on check-six forum: (http://www.checksix-forums.com/) I 1-1
A1-Mc Donnell Douglas F-4D Blk.37-NFM--r1 Level Flight Envelope I 1-2
Alt (ft) Alt (ft) A1-Mc Donnell Douglas F-4D Blk.37-NFM--r1 Level Flight Envelope 65, 6, 55, 5, Level Flight Enveloppe Full AB Clean GW = 36,135 lbs 45, 4, 35, 3, 4xAIM-7E + SUU-23 GW = 39,816 lbs 25, 2, 15, 1, 5, 75 Kts (IAS) from SL to 3,ft 7Kts over..1.2.3.4.5.6.7.8.9 1. 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2. 2.1 2.2 2.3 2.4 65, MILL Power Mach Level Flight Enveloppe MIL Power 6, 55, Clean GW = 36,135 lbs 5, 45, 4, 35, 3, 25, 2, 15, 1, 5, 4xAIM-7E + SUU-23 GW = 39,816 lbs 75 Kts (IAS) from SL to 3,ft 7Kts over..1.2.3.4.5.6.7.8.9 1. 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2. 2.1 2.2 2.3 2.4 Mach I 1-3
A1-Mc Donnell Douglas F-4D Blk.37-NFM--r1 Turn Performance Engine : J79-GE-15 5% internal fuel GW= 39,816 lbs I 1-4
Sustained Turn rate (deg/s) Maximum instantaneous turn rate (deg/s) Turn Rate Summary A1-Mc Donnell Douglas F-4D Blk.37-NFM--r1 Maximum Available Turn Rate 25. 2. 1, 2, 3, 4, 15. Maximum reached without AoA limit (Stall speed) Ng < 8.16 for mach number <.72 Ng < 6.24 for mach number > 1.5 1. 5....2.4.6.8 1. 1.2 1.4 1.6 1.8 2. 2.2 2.4 Mach number 25. 2. Maximum Sustained Turn rate (deg/s) 1, 2, 3, 4, 15. 1. 5....2.4.6.8 1. 1.2 1.4 1.6 1.8 2. 2.2 2.4 Mach number I - 1-5
Sustained Load Factor (Ng) Maximum Available Load Factor (Ng) Load Factor Summary A1-Mc Donnell Douglas F-4D Blk.37-NFM--r1 1. 9. 8. Maximum Available Load Factor 1, 2, 3, 4, 7. 6. 5. 4. 3. 2. Maximum reached without AoA limit (Stall speed) Ng < 8.16 for mach number <.72 Ng < 6.24 for mach number > 1.5 1...2.4.6.8 1. 1.2 1.4 1.6 1.8 2. 2.2 2.4 Mach number 1. 9. 8. Maximum Sustained Load Factor (Ng) 1, 2, 3, 4, 7. 6. 5. 4. 3. 2. 1...2.4.6.8 1. 1.2 1.4 1.6 1.8 2. 2.2 2.4 Mach number I - 1-6
Turn Rate (degree per second) A1-Mc Donnell Douglas F-4D Blk.37-NFM--r1 Turn Performance Sea Level 24. 2G 3G 4G 5G 6G 7G 8G 9G 22. Max. Instantaneous Turn Rate = 21.6 deg/s 2. 18. 16. 14. -6-4 -2 Max. Sustained Turn = 13.7 deg/s 12. 1. +2 8. 6. 4. +4 MAXIMUM AIR SPEED 2. +6. 5 1 15 2 25 3 35 4 45 5 55 6 65 7 75 8 CAS (Kts) I 1-7
Turn Rate (degree per second) A1-Mc Donnell Douglas F-4D Blk.37-NFM--r1 Turn Performance 5, ft 24. 2G 3G 4G 5G 6G 7G 8G 9G 22. 2. Max. Instantaneous Turn Rate = 19.9 deg/s 18. 16. 14. 12. -6-4 -2 Max. Sustained Turn = 12. deg/s 1. +2 8. 6. 4. +4 MAXIMUM AIR SPEED 2.. 5 1 15 2 25 3 35 4 45 5 55 6 65 7 75 8 CAS (Kts) I 1-8
Turn Rate (degree per second) A1-Mc Donnell Douglas F-4D Blk.37-NFM--r1 Turn Performance 1, ft 24. 2G 3G 4G 5G 6G 7G 8G 9G 22. 2. Max. Instantaneous Turn Rate = 18.1 deg/s 18. 16. 14. -6-4 12. 1. -2 Max. Sustained Turn = 1.3 deg/s 8. 6. 4. +2 +4 MAXIMUM AIR SPEED 2.. 5 1 15 2 25 3 35 4 45 5 55 6 65 7 75 8 CAS (Kts) I 1-9
Turn Rate (degree per second) A1-Mc Donnell Douglas F-4D Blk.37-NFM--r1 Turn Performance 15, ft 24. 2G 3G 4G 5G 6G 7G 8G 9G 22. 2. 18. 16. Max. Instantaneous Turn Rate = 16.3 deg/s 14. 12. 1. -6-2 -4 Max. Sustained Turn = 8.8 deg/s 8. 6. 4. 2. +2 +4 MAXIMUM AIR SPEED. 5 1 15 2 25 3 35 4 45 5 55 6 65 7 75 8 CAS (Kts) I 1-1
Turn Rate (degree per second) A1-Mc Donnell Douglas F-4D Blk.37-NFM--r1 Turn Performance 2, ft 24. 2G 3G 4G 5G 6G 7G 8G 9G 22. 2. 18. 16. 14. Max. Instantaneous Turn Rate = 14.6 deg/s 12. 1. -6-4 8. 6. 4. 2. -2 Max. Sustained Turn = 7.4 deg/s +2 MAXIMUM AIR SPEED. 5 1 15 2 25 3 35 4 45 5 55 6 65 7 75 8 CAS (Kts) I 1-11
Turn Rate (degree per second) A1-Mc Donnell Douglas F-4D Blk.37-NFM--r1 Turn Performance 25, ft 24. 2G 3G 4G 5G 6G 7G 8G 9G 22. 2. 18. 16. 14. Max. Instantaneous Turn Rate = 13.1 deg/s 12. 1. 8. 6. 4. 2. Max. Sustained Turn = 6.2 deg/s +2-6 -4-2 MAXIMUM AIR SPEED. 5 1 15 2 25 3 35 4 45 5 55 6 65 7 75 8 CAS (Kts) I 1-12
Turn Rate (degree per second) A1-Mc Donnell Douglas F-4D Blk.37-NFM--r1 Turn Performance 3, ft 24. 2G 3G 4G 5G 6G 7G 8G 9G 22. 2. 18. 16. 14. 12. Max. Instantaneous Turn Rate = 11.5 deg/s 1. 8. 6. 4. 2. -6 Max. Sustained Turn = 5.2 deg/s -4-2 +2 MAXIMUM AIR SPEED. 5 1 15 2 25 3 35 4 45 5 55 6 65 7 75 8 CAS (Kts) I 1-13
Turn Rate (degree per second) A1-Mc Donnell Douglas F-4D Blk.37-NFM--r1 Turn Performance 35, ft 24. 2G 3G 4G 5G 6G 7G 8G 9G 22. 2. 18. 16. 14. 12. 1. Max. Instantaneous Turn Rate = 1.3 deg/s 8. 6. -6-4 4. 2. -2 Max. Sustained Turn = 3.8 deg/s +2 MAXIMUM AIR SPEED. 5 1 15 2 25 3 35 4 45 5 55 6 65 7 75 8 CAS (Kts) I 1-14
A1-Mc Donnell Douglas F-4D Blk.37-NFM--r1 Climb Performance 5% internal fuel GW= 39,816 lbs I 1-15
Climb Angle (deg) Excess Specific Power (ft/s) A1-Mc Donnell Douglas F-4D Blk.37-NFM--r1 Instantaneous Constant Speed Climb Rate 7 65 6 55 5 45 4 35 3 25 2 5, 1, 15, 2, 25, 3, 35, 4, 45, 15 1 5..1.2.3.4.5.6.7.8.9 1. 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2. 2.1 2.2 2.3 2.4 Mach Constant Speed Climb Angle 9. 8. 7. 6. 5. 4. 3. 5, 1, 15, 2, 25, 3, 35, 4, 2. 1....1.2.3.4.5.6.7.8.9 1. 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2. 2.1 2.2 2.3 2.4 Mach I - 1-16
Climb Angle (deg) Excess Specific Power (ft/s) A1-Mc Donnell Douglas F-4D Blk.37-NFM--r1 MIL Power Instantaneous Constant Speed Climb Rate 3 25 2 15 1 5, 1, 15, 2, 25, 3, 35, 4, 45, 5..1.2.3.4.5.6.7.8.9 1. 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2. 2.1 2.2 2.3 2.4 Mach 9. Constant Speed Climb Angle 8. 7. 6. 5. 4. 3. 5, 1, 15, 2, 25, 3, 35, 4, 2. 1....1.2.3.4.5.6.7.8.9 1. 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2. 2.1 2.2 2.3 2.4 Mach I - 1-17
A1-Mc Donnell Douglas F-4D Blk.37-NFM--r1 Acceleration Performances 5% internal fuel GW= 39,816 lbs I 1-18
Time (s) Time (s) Acceleration Diagram A1-Mc Donnell Douglas F-4D Blk.37-NFM--r1 1, 2, 18 Acceleration (Max Thrust AB) 165 15 135 12 1, ft 15 9 75 6 2, ft 45 3 Sea Level 15.3.4.5.6.7.8.9 1. 1.1 1.2 1.3 1.4 1.5 1.6 3, 3, 36, Mach 18 165 15 Acceleration (Max Thrust AB) 3, ft 135 12 15 9 75 6 3, ft 36, ft 45 3 15.3.4.5.6.7.8.9 1. 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2. 2.1 2.2 Mach I 1-19