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Form Data - Rocket allows the user to define a Serde model, and use it to parse the Form Data, and pass it as native rust object to the route handler. Request Guards - the route handlers can contain a special kind of parameters named "Request Guard"s that are meant to prevent the code inside the handler to be called in case a certain condition ...
As with many Soviet rockets, the names of recurring payloads became associated with the launch vehicle itself. The moniker "Proton" originates from a series of similarly named scientific satellites, which were among the rocket's first payloads. During the Cold War, it was designated the D-1/D-1e or SL-12/SL-13 by Western intelligence agencies.
The rocket was 1.4 metres (4 ft 7 in) long, 30.5 centimetres (12 in) in diameter, and had a takeoff weight of 150 kilograms (330 lb). The engine, designed by Arthur Rudolph , used a pressure-fed rocket propellant system burning ethanol and liquid oxygen , and produced 2.9 kN (660 lbf ) of thrust for 16 seconds.
The bodies of both rocket stages are made from stainless steel [21] and are manufactured by stacking and welding stainless steel cylinders. [22] These cylinders have a height of 1.8 m (5 ft 11 in), a thickness of 4 mm (0.16 in) and a mass of 1,600 kg (3,500 lb) each. [22] Domes inside the spacecraft separate the methane and oxygen tanks. [22]
Family of Scatterable Mines (FASCAM) is an umbrella term for a range of systems of the armed forces of the United States, which allows a maneuver commander to rapidly place mines as a situational obstacle; as a reserve obstacle emplacement capability; and to directly attack enemy formations through disrupt, fix, turn, and block.
TOS-1 Buratino (Russian: тяжёлая огнемётная система [ТОС-1], romanized: Tyazhyelaya ognemyetnaya sistema [TOS-1], Heavy Flamethrower System) is a Soviet 220 mm 30-barrel (original system, Object 634 or TOS-1M) or 24-barrel (Object 634B or TOS-1A Solntsepyok) multiple rocket launcher capable of using thermobaric warheads, mounted on a T-72 / T-90 tank chassis.
The test took place on September 15, 2021, at the testing ground of the Military Institute of Armament Technology in Zielonka near Warsaw in Poland. The rocket engine, according to the plan, worked for 3.2 s, accelerating the rocket to a speed of about 90 m/s, which allowed the rocket to reach an altitude of 450 m. [30]
However, with the Type 21/Type 22, the rocket motor is attached to the bomb with a different adapter plate for each type of bomb and the motor does not drop away when it burns out. [2] An adapter sleeve fits into the tail of the warhead and the forward end of the rocket motor and was riveted around the circumference joining the two.