|
CN108953002A
|
|
With the rocket series thrust chamber on single flow head and cooling discharge partition
|
|
WO2018227317A1
|
|
Super large and large rocket thrust chamber for human lunar exploration or mars exploration
|
|
CN107084073A
|
|
Manned moon landing steps on Mars rocket ultra-large type liquid oxygen thrust chamber
|
|
CN107152353A
|
|
New rocket and airship series hydrogen peroxide thrust chamber
|
|
CN106494626A
|
|
Four kinds of high-speed aircrafts with new work engine
|
|
CN105841193A
|
|
Two aerospace turbofan engines
|
|
CN105222159A
|
|
Two kinds have operatic tunes re-generatively cooled formula after-burner and application thereof
|
|
CN104632467A
|
|
Rocket thrust chamber provided with acoustic cavity and applied to supersonic airliner and supply system thereof
|
|
CN103982332A
|
|
Rocket thrust chamber with fuel switching function and supply system of rocket thrust chamber
|
|
CN103775246A
|
|
Hydrogen peroxide/liquid hydrogen gas generator and thrust chamber
|
|
CN102863994A
|
|
Four-component fuel hypergolic with 70%-98% of hydrogen peroxide
|
|
CN1908133A
|
|
Group substituted silanes spaceflight fuel
|
