Method for producing components for rocket construction
DE102006007406B3
Thrust measuring bridge for technical measurement detection of thrust of e.g. aircraft engine, has thrust determining device, which is provided for determination of thrust of engine from parameter
DE102005062030B3
Heat shield for mounting on a heat-radiating article, in particular on a rocket engine
DE102005062092B3
Aggressive storable propellant e.g. hydrazine, receiving and storage tank for operation of e.g. satellite, has tank outlet with connecting-or opening channels and helical channel, where channels connect reservoir with outlet pipe of outlets
WO2006056716A1
Assembly for a spacecraft propulsion system and propulsion system comprising at least one such assembly
EP1674390A1
Ejector for spin-stabilised container
DE102005049686A1
Injector
DE102005035356B3
Fuel tank for storing aggressive media used for powering spacecraft comprises an outlet with holes for connecting an outlet tube to a collecting container
DE102005028584A1
coaxial valve
DE102005021459B3
Mechanical rotation drive with rod-like torsion element
DE102005005158A1
Unfoldable object e.g. weather balloon, inflating method, involves passing of object over gaseous state under pressure and temperature in relation to conditions according to operative environment
DE102004063116B3
Missile ejection device for space craft, has ring units and twisted towing ropes arranged between ring units, and missile holding and guiding units arranged at ring unit connected with structure of space craft
DE102004063115B3
Spin-stabilized vessel dropping device for spacecraft, has central rope roll placed on ring which serves as holding ring, in which vessel is set in translatory motion when vessel, placed on holding ring, rotates along with holding ring
US2005145679A1
Method for brazing ceramic surfaces
DE102004045855A1
Control and / or drive device for a missile
DE102004016593A1
Device for transferring loads
DE102004014618B3
Electrothermal impulse engine
DE102004008681A1
Method for energy transmission by means of coherent electromagnetic radiation
DE102004006665A1
Injection element in coaxial design with two combustion zones
DE102004002543A1
Device for spacecraft for acceleration measurement
