- dual-thrust
- с двумя ступенями тяги
Englsh-Russian aviation and space dictionary. - M.: Military publishing house USSR Ministry of Defence. edited by M. Murashkevich. 1974.
Englsh-Russian aviation and space dictionary. - M.: Military publishing house USSR Ministry of Defence. edited by M. Murashkevich. 1974.
Dual-thrust — In a dual thrust solid fuel rocket motor, the propellant mass is composed of two different types or densities of fuel. In the case of a tandem dual thrust motor, the fuel closest to the rocket nozzle burns fast and the fuel further into the motor … Wikipedia
Dual-Stage 4-Grid — (DS4G) is an electrostatic ion thruster currently under development by the European Space Agency, in collaboration with the Australian National University. A single 20 cm diameter 4 grid ion thruster could operate at 250kW power to produce a 2.5N … Wikipedia
Dual mode propulsion rocket — Dual mode propulsion systems combine the high efficiency of bipropellant rockets with the reliability and simplicity of monopropellant rockets. Dual mode systems are either hydrazine/N2O4, or MMH/hydrogen peroxide (the former is much more common) … Wikipedia
RIM-66 Standard — Infobox Weapon is missile=yes name=RIM 66 Standard MR caption=A RIM 66 Standard MR on an Mk 26 launcher origin= USA type=Medium range surface to air missile used by=United States Navy, Japanese Maritime Self Defense Force, Royal Netherlands Navy … Wikipedia
PL-12 — Infobox Weapon is missile=yes name=PL 12 SD 10 caption=puic| origin= type=Medium range air to air missile used by= manufacturer=CATIC unit cost=$84,000 USD propellant= production date=2002 service=2007 engine=Solid fuel dual thrust rocket motor… … Wikipedia
GTR-18 Smokey Sam — GTR 18 GTR 18 Smokey Sams on launch rails Type SAM simulator rocket … Wikipedia
S-520 — is the designation of a Japanese sounding rocket. The S 520 is a powerful single stage rocket which is optionally equipped with three axis attitude control and a recovery system. It has a capability for launching a 100 kg payload far above 300 km … Wikipedia
Rocket engine nozzle — A rocket engine nozzle is a propelling nozzle usually of the de Laval type used in a rocket engine to expand and accelerate the combustion gases, from burning propellants, so that the exhaust gases exit the nozzle at hypersonic… … Wikipedia
Air-to-air missile — An air to air missile (AAM) is a guided missile fired from an aircraft for the purpose of destroying another aircraft. It is typically powered by one or more rocket motors, usually solid fuelled but sometimes liquid fuelled. Ramjet engines, as… … Wikipedia
S-200 — For the S 200 Minijet see SIPA Infobox Weapon name= S 200 Dvina NATO reporting name: SA 5 Gammon caption= Model of the S 200 missile on its launcher origin= flagcountry|Soviet Union type= Strategic SAM system is vehicle=yes is UK=yes service=… … Wikipedia
9K33 Osa — SA 8 redirects here. For the Apollo flight, see A 104 (SA 8). 9K33 Osa (NATO reporting name: SA 8 Gecko) 9K33 OSA transporter erector launcher and radar(TELAR) … Wikipedia