Supersonic missile seeker lens system using gradient index material for first element lens
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Authors
Davidson, David S.
Advisors
Fuhs, Allen E.
Second Readers
Milne, Edmund A.
Subjects
Missile sensors
Missile aerodynamics
Projectile aerodynamics
Gradient refractive index
Lens design
Conical optics
Conical lens
Guided projectile
Missile aerodynamics
Projectile aerodynamics
Gradient refractive index
Lens design
Conical optics
Conical lens
Guided projectile
Date of Issue
1984-09
Date
September 1984
Publisher
Monterey, California. Naval Postgraduate School
Language
en_US
Abstract
The design of a supersonic missile seeker lens system using an aerodynamically efficient lens, a scanning mirror and detector was accomplished through the use of ray-tracing routines. The design of the first element lens uses a gradient in refractive index to overcome the severe handicap that the pointed shape imposes. This problem had been previously solved for positive orientations of the center of symmetry of the Gradient Refractive Index (GRIN) material with respect to the lens. In this study, the negative orientations are resolved and the lens studies for a range of orientations and strengths of gradient. The best lens in then used in conjunction with the mirror and detector in a ray-tracing scheme. Such a system was found to be feasible and worthy of further study.
Type
Thesis
Description
Series/Report No
Department
Department of Physics
Department of Aeronautics
Organization
Naval Postgraduate School (U.S.)
Identifiers
NPS Report Number
NPS-67-84-016
Sponsors
Defense Advanced Research Projects Agency (DARPA)
Funding
N622718WE40007
Format
Citation
Distribution Statement
Approved for public release; distribution is unlimited.
Rights
Copyright is reserved by the copyright owner
