Fuel molding comprises a blind hole (4) respectively present on opposite base surfaces (2).

The system has an accessory sample (11) produced from a fuel-lot in addition to a rocket. The sample includes an engine combustion chamber, which is filled with a solid-propellant from the fuel-lot and corresponds to an engine combustion chamber of the roc...

The thermal insulation structure has winding portions (10-12) that are made of resin material and/or elastomer material. The winding axis of the winding portions is set to coincide with a longitudinal axis (15) of a thrust nozzle (3) which is provided with...

The apparatus has two propellant charges (4), where each charge is provided with an igniter (8) and the igniter of one of the charges is initiated independent of the igniter of the other propellant charger. A retaining device for receiving incineration par...

The device has a gas generator (1) i.e. single or dual-fuel gas generator, operated by combustion of fuel (7) i.e. explosive material, present in a fuel tank (8). Amount of fuel supplied during the combustion depends on pressure present in a buoyancy tank ...

The device (1) has a pressure tight barrier (7) for separating two exothermically reacting substances (5, 6), where one of the substances lies below a release temperature of the device in a liquid aggregate state, and the other substance lies at the releas...

The missile has a ramjet with a combustion chamber (1) whose inner side is lined with a thermal insulation layer. Cylindrical combustion chamber housing has air inlet openings (4, 5) that are arranged in rows. Fuel rich hot gas formed from a high-energy so...