myanmarsniper
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Hi Guys, any comparisons? 
MiG29 SMT Vs Gripen NG
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jarves
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When you post a comparison thread,be sure that you post there specs also.I will try to find for MiG29SMT,you try to find for Gripen NG.Hi Guys, any comparisons?
Skull and Bones
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Yes, both flies.
HariPrasad
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In Dog fight, Mig 29 is unparallel and beatable by Su 30 onward series and F 22 only. NG is also a very good plane but I do not think that it can stand against mig in close combat. My 2 cent.
Hi guy,
Where is your scary avatar having a scratch on face?
Hi guy,
Where is your scary avatar having a scratch on face?
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jarves
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MIG29SMT
Crew: 1
Number of Engines: 2
Dimensions
Height: 4.70 meter
Length: 17.3 meter (57 foot)
Main Gun Caliber: 30 millimeter
Wingspan: 11.4 meter (37.4 foot)
Performance
Ceiling: 17,700 meter (58,071 foot)
Max Range: 6,000 kilometer (3,240 nautical mile)
Min Range: 2,100 kilometer
Speed
Top Speed at High Altitude: 830 mps (2,989 kph)
Weapons of the MiG-29
The MiG-29 fighter is equipped with seven external weapon hardpoints. The aircraft can carry: up to two R-27 air-to-air medium-range missiles; six R-73 and R-60 air-to-air short range missiles; four pods of S-5, S-8, S-24 unguided rockets; air bombs weighing up to 3,000kg and 30mm built-in aircraft gun with 150 rounds of ammunition.
The R-27 medium-range air-to-air missile is supplied by the Vympel State Engineering Design Bureau, based in Moscow. The R-27 is available in two configurations: the R-27R, which has a semi-active radar homing head and inertial navigation control with a radio link and the R-27T missile, which is fitted with an infrared homing head.
The missile can intercept targets with a speed of up to 3,500km/h at altitudes from 0.02-27km, and the maximum vertical separation between the aircraft and the target is 10km.
The Vympel R-73 missile is an all-aspect, short-range air-to-air missile known by the Nato codename AA-11 Archer. The missile has cooled infrared homing and can intercept targets at altitudes between 0.02 and 20km, target g-load to 12g, and with target speeds to 2,500km/h.
The Vympel R-60 (Nato codename AA-8 Aphid) short-range air-to-air missile can engage targets manoeuvring at an acceleration up to 12g. The R-60M has an expanded range of target designation angles to ±20°, a heavier warhead and an upgraded infrared homing head with photodetector cooling.
Targeting systems
The aircraft is equipped with an information and fire control radar system comprising: an N-019 radar developed by Phazotron Research and Production Company, Moscow; an infrared search and track sensor; a laser rangefinder and a helmet-mounted target designator.
For longer-range air combat, the MiG-29 uses radar guidance for the R-27 missile.
Thales TopSight-E helmet-mounted sight and display (HMDS) is being fitted to aircraft for the Indian Navy. Integration phase of the upgrade encompassing ejection seats, weapon delivery and navigation system was completed in November 2009. Thales will also supply TOTEM 3000 Inertial Navigation and GPS.
MiG-29 engines
The MiG-29 is equipped with two RD-33 turbofan engines.
"The mission of the MiG-29 is to destroy hostile air targets within radar coverage limits and to destroy ground targets."
The MiG-29 is the world's first aircraft fitted with dual-mode air intakes. During flight, the open air intakes feed air to the engines.
While moving on the ground, the air intakes are closed and air is fed through the louvres on the upper surface of the wing root to prevent ingestion of foreign objects from the runway. This is particularly important when operating from poorly prepared airfields.
The engines provide a maximum speed of 2,400km/h at altitude and 1,500km/h near the ground and the service ceiling is 18,000m. The maximum range at altitude is 1,500km and 700km near the ground. RD-33 engines for Indian Air Force MiG-29 aircraft are to be license-built in India, under an agreement signed in January 2007.
Performance of the MiG-29 Fulcrum
The MiG-29 can climb at the rate of 330m/s. The maximum and cruise speed of the aircraft are 2,400km/h and 1500km/h, respectively. The ferry range is 2,100km. Its range and service ceiling are 1,430km and 18,000m respectively.
The aircraft weighs around 11,000kg and its maximum take-off weight is 18,000kg.
MiG-29 Fulcrum Fighter Bomber - Airforce Technology
Crew: 1
Number of Engines: 2
Dimensions
Height: 4.70 meter
Length: 17.3 meter (57 foot)
Main Gun Caliber: 30 millimeter
Wingspan: 11.4 meter (37.4 foot)
Performance
Ceiling: 17,700 meter (58,071 foot)
Max Range: 6,000 kilometer (3,240 nautical mile)
Min Range: 2,100 kilometer
Speed
Top Speed at High Altitude: 830 mps (2,989 kph)
Weapons of the MiG-29
The MiG-29 fighter is equipped with seven external weapon hardpoints. The aircraft can carry: up to two R-27 air-to-air medium-range missiles; six R-73 and R-60 air-to-air short range missiles; four pods of S-5, S-8, S-24 unguided rockets; air bombs weighing up to 3,000kg and 30mm built-in aircraft gun with 150 rounds of ammunition.
The R-27 medium-range air-to-air missile is supplied by the Vympel State Engineering Design Bureau, based in Moscow. The R-27 is available in two configurations: the R-27R, which has a semi-active radar homing head and inertial navigation control with a radio link and the R-27T missile, which is fitted with an infrared homing head.
The missile can intercept targets with a speed of up to 3,500km/h at altitudes from 0.02-27km, and the maximum vertical separation between the aircraft and the target is 10km.
The Vympel R-73 missile is an all-aspect, short-range air-to-air missile known by the Nato codename AA-11 Archer. The missile has cooled infrared homing and can intercept targets at altitudes between 0.02 and 20km, target g-load to 12g, and with target speeds to 2,500km/h.
The Vympel R-60 (Nato codename AA-8 Aphid) short-range air-to-air missile can engage targets manoeuvring at an acceleration up to 12g. The R-60M has an expanded range of target designation angles to ±20°, a heavier warhead and an upgraded infrared homing head with photodetector cooling.
Targeting systems
The aircraft is equipped with an information and fire control radar system comprising: an N-019 radar developed by Phazotron Research and Production Company, Moscow; an infrared search and track sensor; a laser rangefinder and a helmet-mounted target designator.
For longer-range air combat, the MiG-29 uses radar guidance for the R-27 missile.
Thales TopSight-E helmet-mounted sight and display (HMDS) is being fitted to aircraft for the Indian Navy. Integration phase of the upgrade encompassing ejection seats, weapon delivery and navigation system was completed in November 2009. Thales will also supply TOTEM 3000 Inertial Navigation and GPS.
MiG-29 engines
The MiG-29 is equipped with two RD-33 turbofan engines.
"The mission of the MiG-29 is to destroy hostile air targets within radar coverage limits and to destroy ground targets."
The MiG-29 is the world's first aircraft fitted with dual-mode air intakes. During flight, the open air intakes feed air to the engines.
While moving on the ground, the air intakes are closed and air is fed through the louvres on the upper surface of the wing root to prevent ingestion of foreign objects from the runway. This is particularly important when operating from poorly prepared airfields.
The engines provide a maximum speed of 2,400km/h at altitude and 1,500km/h near the ground and the service ceiling is 18,000m. The maximum range at altitude is 1,500km and 700km near the ground. RD-33 engines for Indian Air Force MiG-29 aircraft are to be license-built in India, under an agreement signed in January 2007.
Performance of the MiG-29 Fulcrum
The MiG-29 can climb at the rate of 330m/s. The maximum and cruise speed of the aircraft are 2,400km/h and 1500km/h, respectively. The ferry range is 2,100km. Its range and service ceiling are 1,430km and 18,000m respectively.
The aircraft weighs around 11,000kg and its maximum take-off weight is 18,000kg.
MiG-29 Fulcrum Fighter Bomber - Airforce Technology
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Skull and Bones
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This pic is meaningful, we scientists are that fish, and we try to answer the myriad queries of the universe with what we have in the observable domain, that is, the fish bowl.
jarves
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Gripen NG
* Length: 14.1 m
* Span: 8.4 m
* Height: 4.5 m
* Empty weight: 5700 kg
* Normal take off weight: 8500 kg in fighter configuration
* Payload: 6300 kg
* Fuel, internal: 4140 litres approx
* External: 3800 litres
* Max take off weight: 16000 kg
* Range: 3500 km ferry range
* Max speed: Mach 2
* t/w 22000 >26000nm
*thrust vectoring (maybe for new generention)
* Acceleration: M 0.5 to M 1.1 at low altitude in 30 s (old engine)
* Turn performance: 9 G sustained, G onset rate at least 6 G/s (1-9 G in 1.2 s), min -3 G, 20+ deg/s sustained, 30 deg/s instantaneous
Fuel fractions (Full internal fuel in liter/full internal fuel in liter+ empty weight in kg):
Gripen NG (~3150/3150 + 7100): 0.31
Thrust to weight ratio (Thrust in kg/Full internal fuel in liter+ empty weight in kg + 4*BVR, 2*WVR ~1000 kg)
Gripen NG (11975/3150 + 7100 + ~1000): 1.06
Engine: Volvo Aero RM12 (developed from GE F404 with the changes being at least new fan, afterburner flame holder and accessories, partly to make it more suitable to a single engine aircraft)
Max thrust: approx 54 kN, 80.5 kN with reheat, airflow 68 kg/s, compression ratio 27.5:1, mass 1055 kg, overall length 4.04 m, diameter 0.884 m, inlet diameter 0.709 m
Jas 39 Gripen NG
* Length: 14.1 m
* Span: 8.4 m
* Height: 4.5 m
* Empty weight: 5700 kg
* Normal take off weight: 8500 kg in fighter configuration
* Payload: 6300 kg
* Fuel, internal: 4140 litres approx
* External: 3800 litres
* Max take off weight: 16000 kg
* Range: 3500 km ferry range
* Max speed: Mach 2
* t/w 22000 >26000nm
*thrust vectoring (maybe for new generention)
* Acceleration: M 0.5 to M 1.1 at low altitude in 30 s (old engine)
* Turn performance: 9 G sustained, G onset rate at least 6 G/s (1-9 G in 1.2 s), min -3 G, 20+ deg/s sustained, 30 deg/s instantaneous
Fuel fractions (Full internal fuel in liter/full internal fuel in liter+ empty weight in kg):
Gripen NG (~3150/3150 + 7100): 0.31
Thrust to weight ratio (Thrust in kg/Full internal fuel in liter+ empty weight in kg + 4*BVR, 2*WVR ~1000 kg)
Gripen NG (11975/3150 + 7100 + ~1000): 1.06
Engine: Volvo Aero RM12 (developed from GE F404 with the changes being at least new fan, afterburner flame holder and accessories, partly to make it more suitable to a single engine aircraft)
Max thrust: approx 54 kN, 80.5 kN with reheat, airflow 68 kg/s, compression ratio 27.5:1, mass 1055 kg, overall length 4.04 m, diameter 0.884 m, inlet diameter 0.709 m
- 9 G sustained with high onset rate, at least 30 s after 6 G/s and at least 7 G after a gradual (0.1 G/s) onset without anti-G straining manoeuvre
- Biological and chemical warfare protection
- High altitude protection, including explosive decompression
- Arctic climate and cold water survival
- High temperatures (fire) protection both in cockpit and on the ground
- Air blast protection for ejection speeds up to 600 kt
- Thermal protection
Jas 39 Gripen NG
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HariPrasad
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But i recognize you by that picture only.
Very Philosophical. Any new development string theory?
Skull and Bones
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I'm not in string theory, i'm in Nanoelectronics and Plasmonics.
HariPrasad
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Skull and Bones
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I'm enthusiastic about it, but so much is going around at university level not getting media attention. I'll try to post good articles on it soon.
HariPrasad
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Awesome!!!!!!!!
LCA MK2 will have by and large same specification. Engine of MG seems too week. it should also have an engine like LCA MK2 to give it a stunning performance.
Oh thanks man.
jarves
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How Mig29SMT's radar fairs compared to Gripen NG?? what about BVR fight bw them.
HariPrasad
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