1. Mig-29 A Flight Model data

2. Section A : Mig-29 A (9.12) data

3. Dimensions Lenght: 17,32m Height: 4,73m Wingspan: 11,36m
Wing area: 38,056m^2
Overall lift area: 60,890m^2
Wing incidence: 0deg.
Anhedral: 3deg.
Wing aspect ratio: 3,339:1
Tailplane span: 7,78m
Tailplane area: N/A
Tailplane aspect ratio: N/A
Distance between fins: 3,38m
Fin area: N/A

4. Weight and Engine Weight Motorization Empty weight equipped: 10 900kg
Take-off clean: kg
Normal take-off(2x R-27, 4x R-60 no drop tank): kg
Maximum take-off: kg
Maximum landing weight: kg
Maximum internal fuel: 4 870L at 0,78kg/m^3 specific density = 3 700kg.
Maximum external fuel: 1 centreline drop tank of 1 600L capacity for 1 250kg.
In-flight refuelling: none
Motorization
Engine type: 2x Klimov/Sarkisov RD-33 low bypass ratio turbofans.
Maximum dry thrust at S/L: 98,84kN or kgp.
Maximum afterburning thrust at S/L: 162,80kN or kgp.
Specific Fuel Consumption dry: 21,81g/kN
Specific Fuel Consumption afterb.: 59,84g/kN

5. Performance Never exceed speed S/L: 1 480kph(M1,21)
Never exceed speed m: 2 450kph(M2,00)
Maximum operating mach number S/L: MMo 1,2(1 480kph)
Maximum operating mach number m: MMo 2,3(2 815kph)
Maximum climb rate (NTOW): m/min.
Service ceiling: m
Stalling speed m NTOW: 240kph
Landing speed at NTOW: 250kph
Landing speed at MLW: 270kph
Unstick speed at NTOW: 260kph
Unstick speed at MTOW: 290kph
Landing run NTOW w/ chute: 660m
Landing run NTOW: 900m
Take-off run NTOW w/ AB: 250m
Take-off run NTOW: 550m
Max operating alpha: 26deg.
Instantaneous turn rate: 26deg./s
Sustained turn rate : 23deg./s
Max operating g loading below M0,85: +9, -2,25
Max operating g loading above M0,85: +7, -2,25

6. Miscellenous Wing loading(W/S) clean: 368kg/m^2 W/S NTOW: 410kg/m^2
W/S MTOW: 483kg/m^2
W/S at end of combat radius(NTOW): 228kg/m^2
Overall loading clean: 230kg/m^2
Overall loading NTOW: 256kg/m^2
Overall loading MTOW: 303kg/m^2
Overall loading at end of combat radius(NTOW): 142kg/m^2
Ferry range(w/ drop tank): 2 100km
Combat radius clean lo-lo-lo: 535km
Combat radius clean hi-hi-hi: 1 250km
Combat radius NTOW lo-lo-lo: 450km
Combat radius NTOW hi-hi-hi: 900km
Combat radius MTOW lo-lo-lo: 670km
Combat radius MTOW hi-hi-hi: 1 380km
Endurance clean 200m: 1h00min
Endurance clean m: 1h20min
Endurance NTOW 200m: 0h50min
Endurance NTOW m: 1h10min
Endurance MTOW 200m: 1h11min
Endurance MTOW m: 1h40min

7. Section B : Free Falcon 3 Flight Model

8. FF3
Level Flight Envelope

9. FF3
Acceleration (1/2)

10. FF3
Acceleration (2/2)

11. FF3
Maximum G Load

12. FF3
Sustained G Load

13. FF3
Roll Rate

14. My 2cts comments FF3 Flight Envelope : pessimistic
Reasonable under 30,000ft
Maximum mach at 36,000 / 40,000 ft should be 2.35 instead of 2.15
Acceleration : accurate /pessimistic
Very realistic, and if not, (between 20,000 and 35,000ft) rather pessimistic
Maximum Available G : optimistic
Between .5 and 1 G more than real life a low mach (< 0.45 at SL)
Largely over estimated in supersonic and at high altitude
Maximum Sustained G : optimistic
between 1 and 2 G more than real life at sea level and low mach (< 0.45)
Roll Rate: very optimistic
Maximum value largely over-estimated (300 instead of 160)
Negative impact of high dynamic pressure under estimated
IN GENERAL
In level flight configuration, FF3 MIG-29 Fulcrum does not have the advantage versus the Viper (F16-C Blk52) it should have, especially at high altitude
In term of turn rate, the FF3 MIg-29 Fulcrum is closer to the Viper (F16-C Blk52) than it should be. Where the Viper should have a significant advantage

15. Section C : Proposal for Flight Model

16. Level Flight Envelope

17. Acceleration (1/2)

18. Acceleration (2/2)

19. Lift Coefficient

20. Maximum G Load

21. Sustained G Load

22. Roll Rate