27
October 16-18, 2012 Working Group on Space- based Lidar Winds 1 AEOLUS STATUS Part 1: Design Overview

AEOLUS STATUS

  • Upload
    iniko

  • View
    40

  • Download
    1

Embed Size (px)

DESCRIPTION

AEOLUS STATUS. Part 1: Design Overview. Outline of the presentation. Introduction to ALADIN Laser transmitter (TXA) specification Overview on the Laser optical design Overview on the Laser thermo-mechanical design. ALADIN Measurement Geometry. - PowerPoint PPT Presentation

Citation preview

Page 1: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

1

AEOLUS STATUS

Part 1: Design Overview

Page 2: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

2

Outline of the presentation

• Introduction to ALADIN

• Laser transmitter (TXA) specification

• Overview on the Laser optical design

• Overview on the Laser thermo-mechanical design

Page 3: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

3

• Wind measured by Doppler shift of backscattered light

• Single line-of-sight of horizontal wind (HLOS)

• Sun-synchronous orbit• Random error: < 2 m/s• Zero wind bias < 0.4 m/s

ALADIN Measurement Geometry

Page 4: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

4

ALADIN Measurement principle

• Doppler shift of backscattered light vs laser pulse

• Aerosols signal (Mie) predominant at low altitude (< 2kms)

• Molecules (Rayleigh) predominant at higher altitude (> 2 kms)

Page 5: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

5

ALADIN Optical Functional Diagram

RSP principle

Page 6: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

6

T/R Optics

RayleighSpectrometer

Detection Front-end

Chopper

Receiver Equipments

Page 7: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

7

ALADIN Instrument Overview

Page 8: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

8

Instrument Core

Page 9: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

9

The ALADIN laser Transmitter (TXA)

Parameter Requirements

Energy/pulse > 120 mJ @ 50 Hz PRF

Wavelength

Polarisation

355 nm

Linear, better than 100:1

Beam diameter

Output divergence

7.5 mm

< 400 rad full angle

Pulse duration < 100 ns FWHM

Pulse linewidth < 50 MHz FWHM

Spectral purity 99% of pulse energy within 90 MHz

Frequency stability < 4 MHz rms over the observation time

Tunability + 7.5 GHz for initial adjustment

+ 5 GHz in calibration mode (25 MHz steps, 250 MHz steps)

Tuning accuracy < 1 MHz over 28 min (noise)

< 1.7 MHz rms over 28 min (slow drift)

Page 10: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

10

The ALADIN Laser Transmitter (TXA)

• The ALADIN Laser transmitter is a Nd:YAG Q-switched Master Oscillator Power Amplifier (MOPA), frequency tripled & Injection-seeded.

• It operates in Continuous Mode with a PRF of 50 Hz

• The injection-seeding principle is based on the Ramp-Hold-Fire

Page 11: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

11

The ALADIN TXA Functional Block Diagram

Page 12: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

12

Injection + Master Oscillator section

5 mJ IR energy1 mm @ 1/e2

Rod

Q-Switch

Polarizer

Page 13: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

13

Amplification Section

Input Energy 5 mJ3.4 mm @1/e2

1st pass Output Energy ~50 mJ

2nd pass Output Energy 130 mJ

3rd passOutput Energy 350 mJ (IR)

Page 14: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

14

Harmonic section

350 mJ IR Energy

150 mJUV Energy

200 mJIR + VIS

Page 15: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

15

Laser Opto-Thermo-Mechanical Design description

Page 16: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

16

Reference Laser Head (RLH)

• Based on two Non Planar Ring Oscillators (monolithic design ensures high stability)

• The Reference Laser is stabilized to a low drift resonator

• The beat signal between seeder laser and reference laser is processed by a digital PLL (frequency locking loop)

• The seeder beam is injected in a monomode fiber connected to the PLH

Page 17: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

17

Power Laser Head (PLH) Optomechanical Layout

Page 18: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

18

Power Laser Head (UOB + LOB)

Page 19: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

19

Upper Optical Bench (UOB) of the PLH

Page 20: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

20

Master Oscillator (MO)

• Cavity length is folded by 4 mirrors mounted on an Invar plate•The output coupler, the cavity end mirror (on the rod) and the Invar plate are mounted on the UOB

The piezo-actuator holds the output coupler

Invar plate

Rod & RMax

Page 21: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

21

Pump unit (1)

• Zig-Zag Nd:YAG slab Laser diode pumped in front of the beam TIR for efficient optical energy extraction

• Slab TIR coating LIDT limited @ about 100 MW/cm2

• 1000 W Laser Diodes Stacked Array used @ derated power ( ~700 W)

• Typical lifetime 5.109 shots

LD1 LD3 LD5 LD7

LD2 LD6LD4 LD8

Page 22: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

22

Pump Unit (2)

• The pump unit (PU) is made in copper

• Conductively cooled unit ( with thermal filler to minimize air-vacuum transition effect)

• Operated @ 50 Hz

• About 200 W average Heat dissipation PU longitudinal cross section

Page 23: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

23

PUMP UNIT (3)

Pre-Amp PU installed on the UOB

Page 24: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

24

Harmonic Generation

• LBO crystals used for SHG (25mm) and THG (35mm)

• Type I Phase Matching for SHG, Type II Phase Matching for THG

• Heater controlled crystal temperature higher than 30oC

Page 25: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

25

UOB Power Laser Head (PLH)

Page 26: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

26

LOB Power Laser Head (PLH)

Page 27: AEOLUS STATUS

October 16-18, 2012 Working Group on Space-based Lidar Winds

27

Pump Laser Diodes operation

The heat current will be adjusted according to the formula:to keep constant the distribution of absorbed pump energy in the Nd:YAG rod and slab (same heat dissipation @ laser diode => same emission wavelength)