The invention relates to a push-condensing integrated high-resolution space optical load ultra-light carbon
fiber truss support structure. The structure comprises an adjusting
gasket, a secondary lenschamber, a truss rod, a
metal embedded part and a support ring. A boss at the upper end of the adjusting
gasket is an installation plane of a
secondary mirror component, and a boss at the lower end of the
metal embedded part is an installation plane of a truss and a
primary mirror component. The adjusting
gasket, the secondary lens chamber and the
metal embedded part are made of
titanium alloy materials, and the truss rod and the support ring are made of
carbon fiber composite materials. The cross section of the truss rod is concentric-square-shaped, and the cross section of the support ringis concave-shaped. The truss support structure is less than 2.2 kg in total
mass and is 1 / 3-1 / 2 times of the
mass of a traditional metal truss. The truss support structure is simple, light in weight,good in strength, rigidity,
structural stability and other index characteristics, can
resist the influence of a complex mechanical environment on a space optical load in the transmitting process, ensures the position relation among optical elements, and meets the requirement of the push-condensing integrated high-resolution space optical load on the support structure.