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Work on this design began in 1935 and production commenced in 1943. 1.9 meters long, the bomb is an armor-piercing design, with a thick forged steel nose. The bomb attained a speed of about 100 meters per second when launched. The principal drawback was the small 3.5-kilogram bursting charge. Type 5 No.1 Mk 9 Mod 1 15 kg (33 lb)
Pinaka (lit. ' Bow ') is a multiple rocket launcher produced in India and developed by the Defence Research and Development Organisation (DRDO) for the Indian Army.The system has a maximum range of 45 km (28 mi) for Mark-I Enhanced [7] and 90 km (56 mi) for Mark-II ER version, [8] and can fire a salvo of 12 HE rockets per launcher in 44 seconds.
A mouse trap type electrical impact fuze, 1 second delay, detonation sets off filler M228 M69 Training fuze with functional fuze to train on the 4–5 second delay C12 M25/A1/A2 Integral detonating fuze, 1.4–3 second delay, detonator bursts body scattering agent M200/A1 M6/A1, M7, M8, M14, M16, M18 A mouse trap type igniting fuze.
The MK 1 is a time-fused fragmentation grenade and has 32 serrations on it. To start the fuse, the user has to pull the safety pin, then push off the cap on top of the grenade. Right before throwing, the user has to move the switch on the lever away from the grenade in order to start the fuse.
Astra Mk-1 fired from Su-30MKI. Preliminary work on Astra Mk-1 had begun by 1990 with the completion of a pre-feasibility study. [28] It was revealed to the public for the first time at Aero India 1998. [29] It was described as an elongated Matra Super 530D with a smaller diameter in front of the wings. [30]
The Mk 7 Mods 3, 4, and 6 bomb dispensers have the Mk 339 Mod 1 fuze, which provides the pilot with in-flight selection of the fuze function time. The Mk 7 Mod 4 bomb dispenser differs from the Mk 7 Mod 3 by modifying the dispenser and giving interface capabilities with a wider range of military aircraft.
The missile contains a 1.4-kilogram (3.1 lb) warhead with a contact fuze and a single-stage solid-rocket motor that accelerates the missile to about 650 metres per second (2,100 ft/s), about Mach 2. Engagement time to the maximum effective range is about 13 seconds.
The Mark 1, and later the Mark 1A, Fire Control Computer was a component of the Mark 37 Gun Fire Control System deployed by the United States Navy during World War II and up to 1991 and possibly later. It was originally developed by Hannibal C. Ford of the Ford Instrument Company [1] and William Newell.