|
DE102017102160A1
|
|
Apparatus and system for controlling missiles and kill vehicles operated with gelled propellants
|
|
DE102017100058A1
|
|
Device for stabilizing a fuel assembly with formation of outflow channels
|
|
DE102016121081A1
|
|
Ausstosstriebwerk as annular combustion chamber with device for stabilizing a fuel assembly to form outflow channels
|
|
DE102016107420A1
|
|
Thermal insulation for thermal insulation of an endothermic reaction zone - fibers
|
|
DE102016107416A1
|
|
Thermal insulation for thermal insulation of an endothermic reaction zone - migration barrier layer
|
|
DE102016105251A1
|
|
High-strength space-saving wedge connection of attachments to missile structures
|
|
DE102016101560A1
|
|
Transverse thrust device for active web and attitude control of missiles
|
|
DE102015120196A1
|
|
Propellant reinforcement with fabric insert, fuel reinforcement
|
|
DE102015106822A1
|
|
Motor drive with high boost / sustain thrust ratios
|
|
DE102014115722A1
|
|
Integrated missile propulsion system
|
|
DE102014115721A1
|
|
Active braking of an exhaust engine
|
|
DE102011056581A1
|
|
Gel-shaped fuel
|
|
DE102011115812A1
|
|
Procedure for lifetime monitoring of rockets and accompanying sample to carry out the same
|
|
DE102011018667A1
|
|
Device for the mechanical connection of an actuator with an axially driven by an actuator thrust element
|
|
DE102009019916A1
|
|
Missile with a ramjet engine
|
