That's norm. If anything goes wrong during reentry and the warhead disintegrates, you would require buffer zone.Why so much Large splash zone unless it is MIRV.
That's norm. If anything goes wrong during reentry and the warhead disintegrates, you would require buffer zone.Why so much Large splash zone unless it is MIRV.
from the video cant understand whether it was canisterised or not, although the initial slow launch could be because of being canisterised but am not sure. if anyone can shed some light please do soReveals quite a lot of info about the missile like 50 second burn time for first stage.
Bahut late ho gaye ho miya
Who the heck names these equipment.
Our favourite Bund Busting Device MK2 too has been transferred to Economic Explosives Ltd.
Mark2? What about Mark 1. Is Mark 1 in production?
It must be a mistake , there is no mk2Mark2? What about Mark 1. Is Mark 1 in production?
Agni 1p can be our own carrier killer.
1. Agni V is having CEP of 100m.
2. Agni 1P can hit moving targets.
Ya'll Nibbiars
he should have added some tamil , urdu and malayalam too , that way nobody can understand anything.
Our favourite Bund Busting Device MK2 too has been transferred to Private Sector .
Bahi kankal , wut ?
Bund cum g##d blasting device
Who the heck names these equipment.
IIRC this was shown in Aero India 2021 (or was it Def Expo 2020?). That’s one ugly mother UAV .Was this posted before ?
View attachment 116401
A Medium Altitude Tactical Reconnaissance Unmanned Aerial Vehicle is being designed and devel- I oped through the IITK-BEML collaboration. The UAV being designed is of medium weight class, with a maximum takeoff weight of 30 kg and will possess short take-off and landing capabilities. Powered with a hybrid power plant with a military grade engine, this UAV will achieve 8+ hours of endurance, with a service ceiling of 5 km and a maximum speed of 40 m/s. The craft will be structurally robust to handle 3G manoeuvres and will be equipped with state-of-the-art surveillance systems. Safety of the UAV against mission failure due to aerodynamic loss of control will be ensured through a robust autopilot.
...