SMOTOR has developed a three-stage power system for a fast response rocket with a 200Kg payload capacity for LEO orbitMain features:Low cost, high reliability, fast responseMain technical indicators:Diameter: 1400mm take-off mass: 28tHeight: 17m Carrying capacity: 200kg(LEO)
The independently developed orbit attitude control power system includes 25N, 200N, 700N, 2000N and other existing product sequence, and can be flexibly customized 10N~10kN thrust orbit attitude control engines according to customer requirements, which can provide accurate attitude adjustment, velocity correction and orbit maintenance services for carrier rockets, satellites and other space vehicles.Master core technology …
Hyperbola-2 is a small liquid launch vehicle with a two-stage series configuration, which is used to launch small satellites. Hyperbolo-2 has a length of 28m, a diameter of 3.35m first-stage arrow body and 2.25m second-stage arrow body, a takeoff thrust of 106t and a low-earth orbit carrying capacity of 1.9 tons.Hyperboloid 2 carrier rocket uses …
Product description:The Mosasaur I vacuum rocket engine is a gas generator cycle vacuum pump-pressured liquid rocket engine with liquid oxygen/liquid methane as propellant. Based on the Mosasaur I as the base platform, the Mosasaur I is evolved by replacing the large area specific nozzle extension section.Product index:Vacuum thrust: 700kN (about 70 tons of force)Vacuum specific …
The “Xingtu I” rocket is a small solid commercial carrier rocket developed by Beijing Xingtu Exploration Technology Co., Ltd. for launching tiny satellites.Length: 21mLoad capacity: 240kg 500kmSSOTake-off weight: 30tDiameter: 1.4m
Propellant combination: non-toxic at room temperaturePressurizing gas: nitrogenThrust variety: CustomizableGround specific impulse >220s
Detonation engine (including spark series, sky Fire series and Earth Fire series)Basic parameterMaximum state: (ISA+15℃)Thrust kgf(kN) 320(3.1)Oil consumption rate kg/(kgf·h)(kg/(kH·h)) XXOverall sizeMaximum engine diameter mm XXLength mm XXFlight altitude: 4~10kmFlight requirement: XXFlight speed: high altitude parallel ≥1Ma, sustained level flight ≥120sTakeoff weight: ≤300kgMaximum task load: XX
“Lingyun” is the first liquid rocket engine launched by Kyushu Yunjian for the commercial space market. It is the first liquid engine product born in the domestic space field that has the capability of multiple starts, depth variable thrust, and support rocket recovery and reuse. Excellent multi-start capability and 20%-100% measured variable thrust performance, through …
Product description:The Tianfalcon 150N bicomponent engine is mainly used for orbit transfer of spacecraft, attitude control and final stage attitude control of missile weapons using green nitrous oxide/methylhydrazine as propellant.Product index:Propellant: MON-3/MMH;Chamber pressure: 1.8MPa;Vacuum ratio: 9:2870NS /kg;Starting acceleration: T90≤15ms;Shutdown acceleration: T10≤12ms;Maximum working time: 500s;Cumulative working hours: 9:28 so 5000s;Cumulative number of operations: 9:28 so 10,000;Product …
