n93-20137 a semiconductor bridge ignited hot gas piston

Post on 09-Jan-2022

3 Views

Category:

Documents

0 Downloads

Preview:

Click to see full reader

TRANSCRIPT

N93-20137

A Semiconductor Bridge IgnitedHot Gas Piston Ejector PillJ

M. C. Grubelich and R. W. Bickes, Jr.

Explosive Components Department 2513

Sandia National Laboratories

Albuquerque, New Mexico

Presented by:

D. E. Mitchell

Explosive Components Department Manager

Approved for public release; distribution is unlimited.

R_,'B :2 _ 13:6/4/92

93

Outline

• Concept

• Performance

• Development

• Application

RWB:2513:_/4/92

04

I

0

r..)

0r...p

r..q

o

_Q

0

ilm,_l i

Im,-iI i

i1.,I._ i

i, wl_l i

i,.ul i

;z:0

[.-,

0F-,r._

U3

o_

©0

P.-,

gG

SCB Philoso h ,_

• SYSTEM DEVELOPMENT

- Sensors

- Smart Firing Sets

- Digital Coupling (Wire and Optical)

- Explosive Component

- Smart SCB

• SCB INTEGRATION

- Discrete

- In-situ

• PARTNERING

- Government Facilities

- Private Industry

- Universities

RWB:2513:6/4/92

98

Technolo Transfer ,_

SANDIA - R&D

Technology Transfer

Commercialization, Production and Sales

Government Applications

SCB TechnologiesThiokol

Bulova

Hercules

License

Private Enterprise

SCB TechnologiesThiokoi

BAI

Products

Attitude Control Motors

RAP

UWARS

Air Bags

Blasting

CRADA

WFO

MIPR

RWB:2513:6/4/92

97

oU=_OLu

_Q

Z

Z_-'Z:_<

..IQ

oQ

u.

O8

A

I

O0Ill00n-o.

00 oo_

o_o_

o!_ _

__.z

>'u.IJO0O. OC

O-_4oC_

ZZ

oo_(.3O.3-3¢J_

Z-I. _'1

Z Z o (/)oo_i

0 '

OO0

X

09

r aoammaaagallOISll 1

Llilno mlwlwllllloll J

Z

/

V)LUa

|II|I|I|II|lI||l|_

| I

_llll_ fell-.J

> <

I----.a I,-... I| |

_|II|I|II|||IIIIl|d

,q.

I.UC1.>.I-.-

l|l|INIlI|lIIII|_

I |L.=.. r', r_ r .=-J _.

[ii"'": 1

.... __

L.. ,.............J jXF--

100

i,LI

IDUU)

m

_Z-J

101

ooo

M

m

+o_Mq(/)ZJ

102

CO

f_4

103

O_m

013.>-

mmmU.O0Z

e_F-F-

UJ

m

F-0mo>

00

6

0m

Z-r0uJF-0or>.

LU>u

u%0.J

XW

mmm

00

Z0

F- #'-z ct

Q W _ LUIll O Z.. I

I11 (/) riLl J

o g>--- O0 m,m

_ _o _o_-111 • >13. Ore,3: -- .-X Ou.#-- (I) oOw .jm,m

00

0

104

I I 1 I I

04 O 04 _ (DI I I

(sl!un fueJ_!qJv ) (x)f 6o-i

cO!

CO0

0

OCO

0

<_o

105

0

5W _

om

E

0_

!

J'

o

0I.-

0

0

106

'I"'

ILln_>.I-

o o U.I n_+1

U-I-- >"

OWm

O-r(Jr-t

+1 o +1 o

< <

u.I

0

_ A A

ol- I-- 1:1,..Z Z W

UJ ,-- U.I (/)÷1_ ,-El (/)w:E =_ <_;< < a.

A

V

< A A

_ II:I-- U.l..>- E z _-

_ WW 0

Z A

Omz_

u I-W)_rooo

c__D

107

HERO STUDIES

* Direct RF Injection

- 10MHz-20W

- 200MHz-3W

- 8.9GHz-20W

- 10 Second Injection Times

- Franklin Institue: "Grossly Insensitive"

• NSWC Ground Plane Facility

High Level RF Environments

HF Communications Bands

Radar Frequencies

- Only One Unit Fired (Arc Conditions)

108

R'_,'Bickes:2 SI ]:&/tt92

SATELLITE FIRING SETS

• Multiple Fire

- 2200 micro-Farads

- Charge = 27.4 V

- Four Parallel Outputs

- Bridge Burst Delta t = 5 microseconds

• Single Fire

- 300 micro-Farads

- Charge 16 V

- Series Resistance 0.4 Ohms

- 2.5 mJ

- Function Time - 81 microseconds

_09

SI/ J-onrr o

urn

n u

o

co

LLI

>-i \t-- U _

t-- ZLU LLtLf) L_

_ t--- J,\

c0 LLI\\\\\\\

.u

JLz_

\\\\\\\\\\\\\

tn

co

o

u >-z "_0 --JNI illt-- nULL] Ill_j ZLU t---

!>I era" _ I

"_ '_i I-'- I _- I/ I-Z Lu_ I

_' / _ I -r_ I

n_

tZ:_ "

!11 I--

0,q.

d00

p,-

!11

l-ZIJJZ0n

00

rr<I::EC0m0U)

0oo

112

mut_

l-I.IJ

m

[L

I-rr,<

8

Q.

I-

U U

U I.--

o,___

I0z

0

(.:3

U_

113

O9Z0

n-wlzl

F-_

8

co 28©

cO

I

114

Motivation

• Develop a Low Firing Energy Ejector

• Control Acceleration Profile

• Control Ejection Velocity

• Use a Single Pyro Device for All Applications

115

RWB:2513:6/¢92

Why Use Pyro Actuators? [_

, ENERGY DENSITY

• FUNCTION TIME

116

RWB:2SI3:_/4/92

N-ODWF-

IIc-

EII

n"WZW

0_

W_.ICO

3

c-

111

0r7w

_J

0r7wwo_or)

_g7-

117

W

>-

F-0<

r7<m

m

111_JNN0Z

\

; 18

Results for THKP

• Recover 20% of Total Energy Available

• Losses - Condensed Species, Heat Transfer

RWB:2513:6/4/92

118

Summ,

• SCB - Safe Low Energy Igniter

• Ignite THKP with an SCB

• Use THKP to Pressurize Small Volume

• Vent Pressurized Volume to Eject Mass

• Control Velocity and Acceleration

• Simple Method to Determine Available Energy

RWB:2513:614/92

UJn-

x

O3UJ

_JZ uJ

00 0 rrO9 _- rr"

n m

W0

W

0rr"

m0

121

This page intentionally left blank.

_22

top related