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Optical System Design for CubeSats Optical System Design for CubeSats

Optical System Design for CubeSats - PowerPoint Presentation

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Optical System Design for CubeSats - PPT Presentation

Joseph M Howard Garrett J West Optics Branch Code 551 GSFC NASA Agenda Optical Design Lab ODL Optical Specifications Refractive vs Reflective Freeform Optics Examples 2 Welcome to the ODL ID: 807340

design optical mirror freeform optical design freeform mirror field pupil optics large system lab refractive odl aperture focal bandpass

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Slide1

Optical System Design for CubeSats

Joseph M. Howard, Garrett J. WestOptics Branch, Code 551, GSFC NASA

Slide2

Agenda

Optical Design Lab (ODL)Optical Specifications

Refractive vs. Reflective

Freeform Optics

Examples

2

Slide3

Welcome to the ODL!!

Optical Design Lab (ODL): Goddard Optics Branch, Bldg

5, Room W054

We provide optical design services, and a gateway to the Engineering Technology Directorate (ETD)

Contact: Joe.Howard@nasa.govThe conversation starts with specifications

3

Slide4

Optical Design Specification

What is the NAME

of your mission, the basic concept (one or two sentences), and the top level science requirements ? Are there "competition sensitive" aspects of this study that you need us to be aware?

Are there

s

chedule

constraints ? (e.g. Instrument Design Lab, IDL, or Mission Planning Lab, MPL, run in a few weeks, etc.)

Number

of instruments ? (typically this is just one)

4

Slide5

Optical Design Specification

Conjugates

? Is your object of interest at infinity, which is to be imaged onto a detector? (This case is the most common.)

Aperture

? Is this defined as an Entrance pupil diameter (EPD) ? Or a working F/# ? Is this requirement driven by radiometry (i.e. sensitivity), or resolution (i.e. diffraction limited) ?

Field of view

(FOV)

?

Do you have a detector concept in mind? If so, tell us the pixel size and array size.

5

Slide6

Optical Design Specification

Focal Length or Magnification

? What is your desired Pixel sampling on the object of interest (e.g. sky or ground) ?

O

ptical performance figure of merit ?

Wavelength range

? (i.e. optical

bandpass

)

 If the instrument is a spectrometer, please include desired spectral resolution.

Systems requirements

?

Strongest engineering driver: cost, volume, mass, or performance?

Any optically important mechanisms (e.g. scan or steering mirrors)?

Any significant packaging or mass constraints for this instrument?

6

Slide7

Design Solutions: Refractive

Plot

Aperture (F

/

#) vs FOVRefractive can be more compact

Large

bandpass

may require many lenses for chromatic correction

Mass adds up for complex systems

Glass may be sensitive to radiation environment

Larger field of view capabilityThroughput may be impacted depending on glass transmittance and number of surfaces

LENSES

7

Slide8

Design Solutions: Reflective

Large

bandpass

are easy to accommodate

Larger Fields are challenging to packageUsually higher throughput compared to glassFreeform shapes can help with packaging and performance…

MIRRORS

8

Slide9

Freeform Optics

Definition

: a mirror or a lens with a non-rotationally symmetric surface, typically with large departures from a best-fit spherical surface (many um to mm).

Enables

:

Wider FOV

Better

Image Quality

Smaller

Reduce number of components

Conic Relay

Freeform

Relay

3 mirror

Asphere

Telescope

Traditional Optics

FREEFORM

S

maller

Less mirrors

9

2-mirror Freeform

Slide10

Example System: Focal

2-mirror telescope, 1UField correction lens

UV capable

40 mm Pupil

3D printedE.g. NEAS

10

Slide11

Example System: Afocal

2-mirror afocal

telescope

Pupil imaging concept

UnobstructedInternal Field StopSquare pupilE.g.

BIRCHES,

etc.

11

Slide12

Example: Simple Spectrometer

Refractive objective

Internal Field Stop

Refractive Collimator

Linear GratingRefractive CameraE.g. SHILO

12

Slide13

Example: Wide-Field

Imager

Refractive, 3 U design

80 mm pupil

10 deg fieldCan cover

UV

E.g., CUTIE, GUCI, etc.

13

Slide14

Example: Freeform

2 U 2-mirror focal system

50 mm pupil, deployed

Large Field (3 x 9

deg)F/5Can be folded

Efficient with

space

E.g. XY

Penta

14

Slide15

Example: Freeform

1 U 2-mirror focal system

20 mm pupil, two channel

Large Field (~4x8 degrees)

F/3.2Efficient with spaceE.g. PROVE

15

Slide16

Concluding Remarks

The minimum aperture size of optical instrumentation is often driven by the laws of physics, so miniaturization of optics is often not an option for science applications.

Freeform optics are enabling smaller optical systems of a given aperture with large fields of view

.

If you need help with your optical design, contact the Optical Design Lab (ODL): Joe.Howard@nasa.gov

16