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Naval Research Laboratory June 1, 2001 Electra title page A Repetitively Pulsed, High Energy, Krypton Fluoride Laser Electra Electra Presented by John Sethian NRL M. Friedman M. Myers S. Obenschain R. Lehmberg J. Giuliani P. Kepple JAYCOR S. Swanekamp Commonwealth Tech F. Hegeler Pulse Sciences, Inc D. Weidenheimer

Naval Research Laboratory June 1, 2001 Electra title page A Repetitively Pulsed, High Energy, Krypton Fluoride Laser Electra Presented by John Sethian

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Naval Research LaboratoryJune 1, 2001

Electra title page

A Repetitively Pulsed, High Energy, Krypton Fluoride Laser

ElectraElectra

Presented by John Sethian

NRLM. FriedmanM. MyersS. ObenschainR. LehmbergJ. GiulianiP. Kepple

JAYCOR S. Swanekamp

Commonwealth TechF. Hegeler

Pulse Sciences, IncD. Weidenheimer

Topics this time

Laser GasRecirculator

LaserInput

OutputOptics

Laser Kinetics

Advanced Pulsed Power System (D. Weidenheimer, Titan PSI)

FoilSupport(Hibachi) Amplifier

Window

Cathode

We have looked at 18 types of cathodes/materials

“You have to kiss a lot of frogs to find a prince” Norman Rostoker

Cathode workshop on May 10 at NRL held by F. Hegeler

The bestso far

•Dielectric Fiber-Double Velvet-Other Velvets-Glass

•Carbon-Fiber-Cloth-Foam 100 ppi-Foam 500 ppi-Flock -2% (ESLI)

•Metal/Dielectric-Ceramic/Honeycomb-Metal/ceramic surface flashover-RHEPP-Fine scale RHEPP

•Patched Cathodes-Silicon Carbide-Carbon/Carbon Fiber-Diamond-like Carbon

•CsI Coated Patches-Double Velvet-Carbon/Carbon ESLI-Silicon Carbide

We evaluate cathodes for turn on, uniformity, gap closure and durability

-10

-8

-6

-4

-2

0

0 20 40 60 80

no

rmal

ize

d d

iod

e cu

rre

nt

time (nsec)

Double Velvet Glass FiberCarbon Flock (2%)Carbon FiberCarbon Foam 100 ppiCarbon ClothRHEPPHoneycomb/Ceramic

0.5

0.6

0.7

0.8

0.9

1.0

1.1

1.2

1.3

1.4

1.5

UNIFORMITY LONGEVITY

CATHODECurrent Density

Variation (rad. film) No. ShotsChange in V or I

first-last ?Pressure @ end of

run

Double Velvet 6% 500 No 2.00E-04Glass Fiber 25% É . É . É .

Carbon Flock (ESLI) 15% 800 Slight 2.40E-05Carbon Fiber (Eusebio) 41% 3100 No 2.30E-05

Carbon Foam (100 ppi) 19% É . É . É .Carbon Cloth 57% É . É . É .

RHEPP 50% 300 Slight 2.00E-05Fine Scale RHEPP 25% É . É . É .

Honeycomb/Ceramic 32% É . É . É .

time (20 nsec/div)

no

rmal

ize

d d

iod

e im

ped

an

ce

Diode current

Normalized@ t =100 nsec

Double VelvetCarbon Flock (2%)Carbon FiberRHEPP

0 5 10 15 20 25 300

5

10

15

20

25

30

35

Edeposited

(keV/electron)

X (CM)

We are developing the emitter & hibachi as a single system

Baseline Design: Pattern emitter to miss hibachi ribsFlow water through ribs for cooling

Step 1: 1-D Energy deposition profileshows 78.6%deposited in gas @ 500 keVLaser Gas

Watercooled rib

Laser GasKr + Ar

1.33 atm

Emitter

Vacuum

.01”Ti Foil

Foil loading 0.9 W/cm2

e-beam

1. Transmission

2. Foil cooling

3. Pattern the beam (to miss the ribs)

4. Ribs provide a electrically flat anode

5. Beam uniformly pumps laser gas

84% at 700 keV

e-beam

Step 2: CFD analysis of foil shows foil cooling ok with uniform e-beam distribution…but needs work for e-beam in strips (2 x current density)

Solutions:•Decrease rise and fall of beam,•Better Tc materials•Higher allowable temp•and…. experimental verification

Uniform e-beamMax foil temp: 627 F

“Strips” e-beamMax foil temp: 990 F

Measured e-beam heat loadingused as input

Would like Ti foil < 650 F

Step 3: We can pattern the electron beam

Radiachromic Film at anode (5 X Mag)

PATCH CATHODE (3 cm x 3 cm)

STRIP CATHODE(3 cm x 1 cm)

Actual cathode hasfiner spacing andsome sections removed

Step 4: Close spaced ribs may be an “electrically flat” anode

Rib

UniformEmitter

Vac.01”Ti Foil

e-beam1 atm

air

No Anode Foil

0 10 20 30 Amps/cm2

Radiachromic Filmafter hibachi foil (“X”)

Rib

UniformEmitter

Vac

.01”Ti Foil

1 atmair

e-beam

X

1 cm

/div

With Anode Foil

1 mm Wide Band

Ribs can be a ferritic material !X0 10 20 30 Amps/cm2

1 cm

/div

Band Out

Step 5: This hibachi configuration should allow the beam to uniformly pump laser gas

0 5 10 Amps/cm2

Y Radiachromic Film1 “ after hibachi foil (“Y”)

0.5

cm/d

iv

1 mm Wide Band

Rib

UniformEmitter

Vac

.01”Ti Foil

1 atmair

e-beam

Diagnostic Film located 2.5 cm after foil.Beam propagates through full density air

With Anode Foil

Scattering length will decrease with: Higher Z of laser gas as scattering goes as Z2 (Kr = 36, air = 7) Possible use of higher Z foils

We are evaluating “HAVAR” as a hibachi foil material

HAVAR: (Co 42 / Cr 20 / Ni 13 / W 2.7 / Mo 2.2 / Mn 1.6 / C .2 / Fe 19.1 )

Specifications,Compared to Ti:

Ti HAVAR

Density 4.5 8.3

Tensile strength (MPa) 460 1860

Thermal Cond (W/m-K) 22 15

Zeff 22 39

Chemical resistance good Ex*

Melting temp (C) 1660 1480

248 nm reflectivity @ 80 (angle)- after exposure to F2 (lower reflectivity reduces ASE)

Ti > 0.3 HAVAR: TBD

Burst Strength:

Our measurements: * Fluorine resistance undocumented

Ti HAVAR

248 nm refectivity (exp to F2)** >0.3 TBD

Burst Test 1 mil foil (no exp) 500 1100 psi

Burst Test 1 mil foil (no exp) 1100 TBD

Burst test 2 mil foil (exp to F2) 1100 TBD

** lower reflectivity reduces losses (ASE)

Doug WeidenheimerTitan-PSI

onAdvanced Pulsed Power for Electra

Summary of progress since last meeting

Ultimate cathode is still elusive, but have candidates

New Baseline Hibachi design looks good so far, Needs more testing

Advanced Pulsed Power program developing components

Identified three systems that can meet requirementsStarted component development

Advanced photonically triggered switchesEnd of life testing of existing components