FIELD: optical engineering. SUBSTANCE: objective has mirror components one of which is made as concave mirror and the other, as convex mirror mounted for removal from travel of rays for discrete variation of objective optical parameters. Third component is made as lens compensator. Objective is provided with auxiliary lens component the optical axis of which is parallel to optical axis of objective or coincides with it. Optical force ϕa of auxiliary lens component is related to optical force ϕl of lens compensator as ϕa = (1-S′ϕl)/d+S′(1-dϕl) ,, where d is distance between main planes of auxiliary lens component and lens compensator; S′ is distance from lens compensator to focal plane of objective. EFFECT: more effective variation of parameters. 3 cl, 3 dwg, 2 tbl
Title | Year | Author | Number |
---|---|---|---|
SPACE MIRROR-LENS TELESCOPE | 1999 |
|
RU2154293C1 |
SPACE REFLECTING-REFRACTING TELESCOPE | 1996 |
|
RU2115942C1 |
REFLECTOR LENS | 2017 |
|
RU2670237C1 |
CATADIOPTRIC LENS FOR NEAR-INFRA-RED RADIATION SPECTRUM | 1996 |
|
RU2091835C1 |
INFRARED MIRROR-LENS OBJECTIVE WITH DOUBLE FIELD OF VIEW | 2005 |
|
RU2292066C1 |
MIRROR-LENS TELESCOPE LENS FOR A MICRO-CLASS SPACECRAFT | 2022 |
|
RU2798769C1 |
OPTOELECTRONIC CAMERA FOR REMOTE EARTH SOUNDING | 1998 |
|
RU2168752C2 |
OBJECTIVE | 0 |
|
SU1742771A1 |
REFLECTOR LENS | 2010 |
|
RU2415451C1 |
MIRROR ATHERMALIZED LENS | 2018 |
|
RU2680656C1 |
Authors
Dates
1998-04-10—Published
1996-02-20—Filed