The application provides a wide-temperature miniaturized coherent
telescope system, which comprises a spacer ring, a pressing ring, a first lens, a second lens, a
secondary mirror pressing ring, a
secondary mirror seat, a third lens, an adjusting sleeve and a
fiber flange. The application comprehensively considers factors such as
telescope performance, size, weight and environmental adaptability, and selects H-ZF6, H-K9L and H-ZK3 as the optical lens, adopts TC4
titanium alloy material as the structure, compensates each other between the change of the
refractive index, the curvature
radius and the thickness of the optical element with the temperature and the
thermal deformation of the structure, realizes stable work without
temperature control at-40~60 DEG C, re-distributes the tolerance sensitivity of the optical element by using a unique optical design form, only the
secondary mirror needs to be centered and adjusted among the three lenses, which greatly shortens the adjustment period and difficulty, through the additional receiving
field of view of ±0.03 DEG, the focal point can still meet the
system wave aberration requirement of 1 / 20
lambda within the range of 0.13 mm
radius, avoids a complex
fiber adjusting mechanism, and is applied to the field of coherent
wind measurement laser radar.