Launch vehicle parts

Conical, cylindrical and biconical shells for nose cones and launcher instrument bays

sandwich structures consisting of aluminum honeycomb core and CFRP skins

Intended use:

Protection of payload during the atmospheric phase of flight and under ground operation conditions.

They are used in the launchers Proton-M, Rokot, Angara1, 2.

Characteristics:

• Outer diameter – up to 5100 mm;

• Length - up to 4000 mm.

Shells in the form of closed contour cylinder-cone of the launcher front-body section

are sandwich structures consisting of aluminum honeycomb core and CFRP skins.

Intended use:

For the accommodation of instruments. They are used in the launcher KSLV.

Characteristics:

• Outer diameter – up to 2900 mm;

• Length - up to 2300 mm.