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Icy mountains... High altitudes... Freezing Temperatures... Reduced oxygen... Misadventures by enemy... Prepared for all Challenges #TrainingTuesday #IndianArmy #OnPathToTransformation

32,270 просмотров • 2 лет назад •via X (Twitter)

Комментарии: 9

Фото профиля Kaushal
Kaushal2 лет назад

#NoAgniveer

Фото профиля Vishal Mishra
Vishal Mishra2 лет назад

इंडियन army always ready for every tough situation 🙏🙏🙏 salute 🫡🫡🫡🫡

Фото профиля ᏰᎥᏖፈᎧᎥᏁ ❤️🇮🇳
ᏰᎥᏖፈᎧᎥᏁ ❤️🇮🇳2 лет назад

That's why Indian army is love 💕

Фото профиля vasutatha
vasutatha2 лет назад

Was in Spiti for 5 days at less than 4500 meters. Froze. It just gets colder as the wind speed picks up. Our forces live at much higher altitudes, day on day, for months. Vigilant. No escape to a warm mud house, a fire. No description fits the experience. Respects 🙏.

Фото профиля Munnish Puri
Munnish Puri2 лет назад

🇮🇳🇮🇳🇮🇳

Фото профиля गंगापुत्र
गंगापुत्र2 лет назад

जय जवान जय भारतीय सेना जय भारतीय संस्कृति जय हिन्द जय भारतवर्ष 🇮🇳❤️🙏🏼🙏🏼🙏🏼🙏🏼🙏🏼

Фото профиля Deepak Kumar
Deepak Kumar2 лет назад

They are real Khatron Ke Khiladi...

Фото профиля Dipin
Dipin2 лет назад

Change the guns

Фото профиля youth of kashmir 🇮🇳
youth of kashmir 🇮🇳2 лет назад

Jai hind 🇮🇳

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Evaluation Results Note: Technicians translated Russian instrument labels, added U.S. gauges (e.g., accelerometer, temperature probe), checked for booby traps, and modified minor systems (e.g., using standard JP-1 fuel and hydraulic fluid mixtures). Testing and Observations - The MiG was structurally sound, with good workmanship in critical areas but some neglect elsewhere. It had a clean aerodynamic look, negative wing dihedral, large rudder, and wing fences for better low-speed handling. - First flight by Captain Collins; subsequent flights included chase by F-86s, showing the MiG's superior acceleration and climb due to lower thrust loading. - Handling was conventional at medium/low speeds; landing speeds were similar to the F-80 (approach ~120 knots, touchdown ~105 knots). - Armament: Unique quick-swap package with two 23mm and one 37mm cannon under the intake, allowing fast rearming. Fired for only ~6 seconds continuously (vs. F-86's 14 seconds). Tests included strafing runs and static firing; casings/links jettisoned. - Performance data matched prior intelligence remarkably well. Strengths (Desirable Features) - Excellent high-altitude capability (reached 55,000 ft; F-86 max ~51,000 ft). - Superior rate of climb (45,000 ft in 9 minutes vs. F-86's 13 minutes). - Rapid acceleration from low speeds. - Short turning radius (effective in low-speed maneuvers). - Short takeoff/landing distances. Weaknesses (Undesirable Features) - Became uncontrollable above ~Mach 0.94 in dives (recovered only in denser air); F-86 remained controllable at higher speeds. - Slightly lower top speed than F-86 at all altitudes. - Poor handling at high speeds (small ailerons, ineffective elevators → slow roll rate). - Poor lateral-directional stability at high altitudes. - Inadequate cockpit features: poor rear visibility, inadequate defrosting, extreme cabin temperatures (up to 42°C low, freezing high), non-self-sealing fuel tanks, oxygen/cabin systems needing constant attention. - Limited ammunition duration and other equipment quirks. Overall Assessment The MiG-15 was a formidable but inferior fighter compared to the F-86 Sabre. Its advantages shone in climb, altitude, and low-speed maneuverability, but the F-86 excelled in high-speed control, handling, and pilot-friendly systems. The reported 13:1 kill ratio favoring F-86s over MiGs was attributed to superior aircraft design and better-trained pilots. After just 4 days and 11 flights, the MiG's capabilities were fully understood—no secrets remained.

Aviation Archive - Tim Farmer

13,707 просмотров • 7 месяцев назад