41
UNCLASSIFIED AD NUMBER: LIMITATION CHANGES TO: FROM: AUTHORITY THIS PAGE IS UNCLASSIFIED AD0476502 Approved for public release; distribution is unlimited. Distribution authorized to U.S. Gov't. agencies and their contractors; Export Control; 1 Dec 1965. Other requests shall be referred to: Army Engineer Waterways Experiment Station, Vicksburg, MS 39180. This document contains Export Controlled Technical Data. 29 Jun 1973 per DNA ltr

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Page 1: UNCLASSIFIED AD NUMBER: AD0476502

UNCLASSIFIED

AD NUMBER:

LIMITATION CHANGES

TO:

FROM:

AUTHORITY

THIS PAGE IS UNCLASSIFIED

AD0476502

Approved for public release; distribution is unlimited.

Distribution authorized to U.S. Gov't. agencies and their contractors; Export Control; 1 Dec 1965. Other requests shall be referred to: Army Engineer Waterways Experiment Station, Vicksburg, MS 39180. This document contains Export Controlled Technical Data.

29 Jun 1973 per DNA ltr

Page 2: UNCLASSIFIED AD NUMBER: AD0476502

MISCELLANEOUS PAPER NO. 1-754

'\ . ,i

DANNY BOY EVENT PROJECT 1.6: MASS DISTRIBUTION

MEASUREMENTS ,QF CRATER ~JECTA AND DUSiT

L K. D1vi1

A. D. Rooke, Jr.

Page 3: UNCLASSIFIED AD NUMBER: AD0476502
Page 4: UNCLASSIFIED AD NUMBER: AD0476502

•, .~ .. ,. ' . . :-.,··

Unclassified Security Clasaification

DOCUMENT CONTROL DAT A · R&D (Security c/aeelllcetlon al title, body al abatrecl and lndaalnl annotation muet be entered wflen the overall report i• c/aeallledJ

t . O"'llilNATIN G ACTIVITY (Corporate eulhar) 2• l'ICPOl'IT 1£CUl'IITY C LAISIFICATION

u. s. Army Engineer Waterways Experiment Station Unclassified ·-2b Gl'IOUP

Vicksburg, Mississippi J . AIPO .. T TITLE DANNY BOY EVENT Project 1.6: MASS DISTRIBUTION .MEASUREMENTS OF CRATER EJECTA AND DUST ( roR/WT-1815) APPENDIX B: VOI.UMETRIC EQUALITIES OF THE CRATER 4 , DIIC .. tPTtVI NOTIS (Type al raporl and lnc/uelve datH)

I AUTHO .. ;I) (Lael nan,e. llrel n·eme, Initial)

Davis, Landon K. Rooke, Allen D., Jr.

f ... IPO .. T DA Tl , .. TOTAL NO . 01' PAGF.I 17b. NO . 9,, l'll!P,1

December 1965 32 la. CONTl'IACT 01'1 Ol'IANT NO. • •• Ol'IIOINATOl'l'I l'IEPOl'IT NUMBl:1'1(5)

b. lll'IOJllCT NO . Miscellaneous Paper No. 1-754

C , tb. iTHl:l'l l'IJPOl'IT No(I) (Anyathernumbera tllatmaybeaael .. ed le report .

d.

t O. AV A IL A• ILITY /LIMITATION NOTICH

This docwnent is subject to special export controls and each transmittal to for-eign governments or foreign nationals may be made only with prior U. S. Army Engineer Waterways Experiment Station.

approval of the

It, IU,-,-LIMINTA .. Y NOTH 12 - IPONIO .. ING MILITA .. Y ACTIVITY

Defense Atomic Support Agency

Washington, D. C.

11- A• IT .. ACT

The resuits of various previously reported investigations of the Danny Boy event are utilized to compute and compare the volumes of ejected material and volumes attributable to other crater-formation mechanisms. Imbalance of the volumetric contributions is attributed primarily to the wicertainty of the ejecta density in the lip region. Approximately 65 percent of the rock material dissociated by the explosion was pennanently ejected from the crater; less than 2 percent of the ejected material was deposited beyond 3 c~ater radii .from grolllld zero. Comparisons are made with high-explosive.~.ud nuclear detonations in desert alluvium.

DD .~~!~. 1473 Unclassified Security Cla•• lfication

1110 r

Page 5: UNCLASSIFIED AD NUMBER: AD0476502

$

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14 .

Unclassified Security Cl.issifici.ition

KEY WORDS LINK A LINK B

1----- - - ·------ ·· ·-----·- . . ·- · ·· ·-··-·· -

ROLE WT ROLE WT

LINK C · · - - - - - -4 ROLE WT

~ - --. ·-· - -- - - - - . - · - --- - -- ----------- - ·-- ----- - -- ' -- - ---- - - - - - - r-- --- ·--t-- ----11------11

Cratering

Explosion effects

Danny Boy (Project)

INSTRUCTIONS

1. ORIGINATING ACTIVITY: Enter the name and address of the contractor, subcontractor, grantee, Department of De­fenae activity or other or1anlzation (corporate author) is,iuing the reJ,ort.

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.. i{fr.<,::,\ ,. .: ,,;-,/:);;ti;it,•>

• • .i ,:-:;-:-,'

10. AVAILABILITY /LIMITATION NOTICES: Enter any llm­it11t ion11 on further dissemination of the report, other than those imposed by security clasalfication, using standard statements such as:

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Servlcea, Department of Commerce, for aale to the public, lndl• cate this fact and ~nter the price, lf known.

11. SUPPLEMENTARY NOTES: Uae for additional explana­tory notea.

12, SPONSORING MILITARY ACTIVITY: Enter the name of the departmental project office or laboratory aponaorln1 (pay­ing for) the research and development. Include address, 13. ABSTRACT: Enter an abstrac-t giving a brief and factual summary of the document indicative of the report, even though it may also appear elsewhere in the body of the technical re­port. If additional space is required, a continuation sheet sha 11 be attached.

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14. KEY WORDS: Key words are· technically meaningful terms or short phrases that characterize a report and may be used as index entries for cataloii:ing the report. Key words must be selectei' so that no security classiflcatlon is required. lden­fiers, such as equipment model designation, trade name, 'Tlili• tary project code name, geop,raphic location, may be used as key words but will be followed by an indication of technical context. The assignment of links, rules, and weights is optional.

Unclassified Security Classification

t

Page 6: UNCLASSIFIED AD NUMBER: AD0476502

MISCELLANEOUS PAPER NO. 1-751J

DANNY BOY EVENT PROJECT 1.6: MASS DISTRIBUTION

MEASUREMENTS OF CRATER EJECTA AND DUST

POR 1815 (WT), APPENDIX B VOLUMETRIC EQUAL~TIES OF TME CRATER

by

L K. Davis

A. D. Rooke, Jr.

December 1965

Sponsored by

DeFense Atomic Support Agency

Conducted by

· U. S. Army Engineer Waterways Experiment: Station

CORPS OF ENGINEERS Vicksburg, Mi11iuippi

Alllff-MIC VICKIIUIIQ, MIii.

This document is subject to special export controls and each transmittal to foreip 1overnments or forei1n nationals may be made onty with prior approval of U. S. Army En1ineer Waterways Experiment Station.

. .~- ~: : . ' · .. ·ir .. ·.

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Page 7: UNCLASSIFIED AD NUMBER: AD0476502

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ABSTRACT

The results of variou8 previously reported investigations of the

Danny Boy event are utilized to compute and compare the volumes of ejected

material and volumes attributable to other crater-fonnation mechanisms.

Imbalance of the volumetric contributions is attributed primarily to the

uncertainty of the ejecta density in the lip region. Approximately

65 percent of the rock material dissociated by the explosion was perma-

nently ejected fran the crater; less than 2 percent of the ejected material

was deposited beyond 3 crater radii fran ground zero. Comparisons are

made with high-explosive and nuclear detonations in desert ·alluvium.

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_. ,, '

Page 8: UNCLASSIFIED AD NUMBER: AD0476502

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PREFACE

The study reported herein was performed as a supplement to

PORfilT-1815, "Project 1.6: Mass Distribution Measurements of Crater

Ejecta and Dust," for the Danny Boy event of Operation Nougat. The

project was under the direct supervision of Mr. J. N. Strange, Chief of

the Engineering Research Branch, and under the overall supervision of

Mr. G. L. Arbuthnot, Jr., Acting Chief of the Nuclear Weapons Effects

Division, U.S. Army Engineer Waterways Experiment Station (WES).

Me·ssrs • L. K. Davis" and A. D. Rooke, Jr. , prepared both the project report

{POR,/WT-1815) and this appendix.

Analyses of the Danny Boy crater lip lithology and exploratory

drilling operations through the true crater cavity were perfonned by

personnel of the WES Soils Division.

During the preparation and publication of this appendix, Col. John R.

Oswalt, Jr., CE, was Director of the WF,S and Mr. J.B. Tiffany was Technical

Director.

V

Page 9: UNCLASSIFIED AD NUMBER: AD0476502

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CONTENTS

ABSTRACT •••••• PREFACE • • • • . •

• • • . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DEFINITIONS • • • • • . . . . . . . . . . . . . . . . . . . . . .

INTIODUCTION . . . . . . . . . • • • . . . . . • • • Objective ...................... .

CHAPrER B.l B.1.1 B.1.2 B.1.3

CHAPrER B.2 B.2.1 B.2.2

Summary of Previous Investi.gation • • • • • • • • • • • Scope of Present Investigation ••.•.•••••••

RESULTS OF CRATER nNESTIGA.TIONS • • • • • • • • • • Crater Lip Survey ••• Crater Dimensions •••

• • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • •

CHAP.rER B. 3 DISCUSSION • • • • • • • • • • • • • • • • • • • • • B.3.1 Volumetric Relations • • • • • • • • • • • • • • • • • B.3.2 Cavity Formation •••.••••••••••• B.3.3 True Crater Formation •••••••••••••

• • • • • • • •

B.3.4 Ejected Material • • • • • • • • • • • • • • • • • • • B.3.5 Correlation with Previous Experiments ••••• • • • •

CONCLUSIONS AND RECOMMENDATIONS • • • • • • • • • • • CHAPrER B.4 B.4.1 B.4.2

Conclusions ••• Recommendations.

• • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • • •

.. REFERE?«:ES • • • • • . . , • • • • • • • • • • • • • • • • • • • •

TABLES B.3.1 Dimensions and Volumes of Danny Boy Crater Regions • •

FIGURES B.2.1

B.2.2 B.2.3

B.2.4 B.3.1 B.3.2

Lithologic profiles of trench through Danny Boy crater lip • • • • • • • • • • • • • • • • • • • • • • Lithology of the Danny Boy crater interior slope • • • Profiles of average ejecta and upthrust surfaces in crater lip • • • • • • • • • • • • • • • • • • • • • Profile of Danny Boy crater •••••••••••••• Danny Boy crater formation • • • • ·,. • • • • • • • • • Schematics illustrating methods of volumetric computations • • • • • • • • • • • • • • • • • • • • •

, •• 1

!1 ~\,

.''.\\."_,:,-:.( :., .•.

vii

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iii V

ix

1 1 1 2

3 3 3

8 8 9

10 11 16

23 23 23

24

17

4 5

6 7

18

19

Page 10: UNCLASSIFIED AD NUMBER: AD0476502

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B.3.3

B.3.4

l

! (

I f

Average mass distribution of ejecta versus radial distance from GZ . . • . • . . • • Fraction of total ejecta volume as a function of range from GZ . • . . • • • • • . Range of Danny Boy ejecta volumes compared with shots in desert alluvium . . . . • • . .

20

21

22

viii

-~--~- ~ ~ - -·- ., ____ __ .. ' "·, ', . . :~ . .'

Page 11: UNCLASSIFIED AD NUMBER: AD0476502

Apparent crater

Crater cavity

Crater lip

Depth of burst (DOB or Z) (also depth of burial)

Ejecta (throwout)

Fallback

Ground zero (GZ)

DEFINITIONS

The visibl,? crater, bounded at the top

by a plane representing original ground

surface

That portion of the crater which is

initially contained ann which is formed

by vaporization and compression of

earth material surrounding the explo-

sion energy source. Its radius is

designated r C

The distinctly raised portion of the

earth mass immediately surrounding the

apparent crater

Depth below original ground surface of

the effective center of the explosion

energy source where no severe ground

slope is involved. When the slope

cannot be ignored, the shortest dis­

tance from zero point to the ground

surface is used

Earth material pennanently ejected

fran the crater as a resul.t of the

explosion

Dissociated material between the true

and apparent crater bOWldaries.

The hypo- or epicenter of the explosion

ix

,·,.,\ .....

Page 12: UNCLASSIFIED AD NUMBER: AD0476502

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True crat1;?r

Upthrust

Zero point (ZP)

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.

The crater prior to fallback, bounded

at the top by a plane reprr.s enting

original ground surface. It represents

the surface of undissociated material.

Its depth and radius are designated

and respectively

Permanent upward movement of original

ground surface Gurroundinr, the true

crater

The center of the detonation; the effec­

tive center of the explosion energy

source

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Page 13: UNCLASSIFIED AD NUMBER: AD0476502

B.1.1 OBJECTIVE

APPENDIX B

VOLUMETRIC EQUALITIES OF THE CRATER

CHAP.rER B.l

INTRODUCTION

The purpone of this appendix is to compa:.:e the relative significance

of various cratering mechanisms (compression, plastic flowage, ejection,

and vaporization) by studying the volumetric contributions of these

mechanisms to the formation of the Danny Boy crater. Observations are

based on information contained in FOR/WT-1815 (Project 1.6, Event Danny

Boy) and in reports of subsequent investigations by U.S. Anny Engineer

Waterwa;ys Experiment Station (WES) personnel and other researchers.

B.1.2 SUMMARY OF PREVIOUS INVESTIGATION

The Danny Boy event was detonated 5 March 1962 at the U.S. Atanic

Energy Camnission's Nevada Test Site (NTS). The device was buried at a

depth of llO feet in basalt and had a yield of o.43 kt (Reference 1).

The Project 1.6 experimental layout consisted of an array of tar­

paul.ins placed in a concentric circular pattern about ground zero (GZ).

After the shot, when the residual radioactivity pennitted, samples of

ejecta (including dust) deposited on the tarpaulins were recovered,

weighed, and analyzed for particle size. The nearest samples to GZ were

recovered at a radial distance of 310 feet and the most remote at 880 feet.

Mass distribution per unit area and size distribution were tabulated and

shown graphically as functions of radial dis.tance from GZ. The amount of

deposition was found to decrease sharply with distance. Particle size

l

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Page 14: UNCLASSIFIED AD NUMBER: AD0476502

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similarly decreased with distance from GZ, the percentar.;e of fines incr eas­

ing rapidly beyond the 310-foot collector rin~. The r esults of s imilar

experiments were summarized and compared with Danny Boy data by m~ans of

dimensionless plots.

B.1.3 SCOPE OF PRESENT INVESTIGATION

Approximately one year after the completion of Project 1.6, WES

personnel excavated a trench through the Danny Boy crater lip, with tbe

centerline of the trench bearing South 67°30' West from GZ. The purpose

of the trench was to expose the uplifted original ground surface near the

crater edge, permitting an analysis of the composition of the ejecta in

the liTJ. In addition, several slant holes were drilled into the true

crater 1.n order to delineate the radius of the cavity surrounding the zero

point. The location of the cavity surface wa~ determined by ~omparing

core samples recovered from the holes, radiation levels along the hole

lengths, and the presence of glass produced by the fusing of the basalt

around the cavity walls (Reference 2).

The results of these investigations were utilized to compute the

volumes of the lip ejecta, the lip upthrust, and the true crater, includ-

1·.1g the true crater cavity. These volumes were then compared with the

V)lumes of the apparent crater and the ejecta as measured in Project 1.6 .

2

• )'

--------..--.• ~-- --·-· - ,·-------·--·- ··-- ·-...,...._.,.--.,_.. _______________ ,

Page 15: UNCLASSIFIED AD NUMBER: AD0476502

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CHAPTER B.2

RESULTS OF CRATER INVESTIGATIONS

B . 2 • 1 CRATER LIP SURVEY

Figure B.2.1 shows the lithologic profiles of the north and south

sides of the trench excavated through the crater lip. Figure B.2.2 is

a circumferential profile of the interior slope of the crater lip and the

upper portion of the apparent crater, showing the maximum lip height, the

height of upthrust, and the upper l:i.mi t of the fallback material. ,Ari

average height of upthrust of 14.3 feet was determ:iined from the circumfer­

ential profile, and the radial extent of the upthrust, 220 feet, shown in

Figure B.2.1 was assumed to be representative of the entire circumference

of the crater. From this information, an averag1:: profile of the uplifted

ground surface was constructed on the average profile of the crater lip

(ejecta surface) as shown in Figure B.2.3.

The average bulk density of the crater ejecta and fallback was esti­

mated to be 3,620 lb/yd3, based upon ejecta sampling reported in Reference 3.

Based upon References 2 and 4, the in situ density of the basalt is taken

to be 4,250 lb/yd~.

B.2.2 CRATER DIM.mSIONS

Figure B.2.4 is an average cross section of the Danny Boy crater. The

lip dimensions were taken from Figure B.2.3, the radius of the c3vity from

the postshot drilling results, and the apparent and true crater dimensions

and configurations from References 5 and 3, respectively.

3

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B.3.1 VOLUMRI'RIC REIATIONS

CHAPI'ER B.3

DISCUSSION

A number of volumetric equalities for craters have been resolved

from a near-surface cratering study by WF.s (Reference 6). For craters

in soil, these relations are:

Where:

Vt = V dis + V C + V f + V V

V =kV I, e

- V a

+v u

V = V u f

vt = volume of true crater

(B.3.1)

(B.3.2)

(B.3.3)

(B.3.4)

(B.3.5)

vdis = volume (preshot) of material dissociated by the explosion

vc = volume of crater due to compression (canpaction)

vf = volume of crater due to plastic flowage of the medium

v = volume of vaporized material V

P0 , P1 = preshot (in situ) and postshot densities of cratered material, respectively

ve = volume of ejecta

vtb = volume of fallback

va a volume of apparent crater

v, • total volume of crater lip

k a a C<Xlatant representing the fracti<Xl of ejecta.volume contributing to the formation of the crater lip

vu= volume of upthrust region

8-

_______ ,

Page 21: UNCLASSIFIED AD NUMBER: AD0476502

', [

Equations B.3.1 through B.3.4 also apply to craters in rock. Howev~r,

for practical considerations, rock l.s assumed to be incapable of flowing

under a hydrodynamic stress unless the stress ia sufficiently large to

transfonn the material into a liquid state. Since the melting of rock in

a nuclear detonation has been observed to be confined to a thin lining on

the interior of the cavity, there is no signi~icant contribution to the

crater volume by this mechanism, and Equation B. 3. 5 does not apply to a

rock medium.

B. 3 .2 CAVITY FORW': ... vtl

The cavity radius (re) of 36 feet determined from postshot drilling

appears to be consistent with the results of previous underground nuclear

detonations. The Neptune, Blanca, Logan, and Rainier events at NTS created

cavities with scaled radii of 50 .:!: 3 rt/Jt.t1/ 3 (Reference 7). The scaled

cavity radius for the Danny Boy event was 48 rt/kt1/ 3• The scaled cavity

radii of the Danny Boy, Neptune, and Blanca events, all of which vented

( the last by a subsidence mechanism), were 47 or 48 ft/kt1/ 3, while those

of the contained shots, Logan and Rainier, were 50 and 52 rt/kt1/ 3,

respectively.

C-vity growth is related to gross upward movement of the overburden

as well as to compression and vaporization of the medium surrounding the

nuclear device. However, the lower part of the cavity appears to be formed

almost entirely by canpression and vaporization. Since this is the only

volume of canpression applicable to the final crater formation ( the can­

pacted medium surrounding the upper part of the cavity is dissociated upon

venting), v c can be readily estimated once vv has been calculated. The

9

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Page 22: UNCLASSIFIED AD NUMBER: AD0476502

.. ,,•, .

volume of vaporized rock for the Danny Boy crater is given in Reference 2

as about J2 cubic yards, an insignificant quantity in comparison with the

uncertainties existi.ng elsewhere in the volumetric computations. If it is

assumed that half of the vaporized material came from the lower part of the

cavity,

= 3,610 yd3 l V

(B.3.6)

Any possible contribution by compression in the sides of the true crater

above the cavity is ignored in this procedure.

B.3.3 TRUE CRATER FORMATION

A general widerstanding of the probable mechanics of crater formation

is necessary to an analysis of the crater volumes created. Figure B.3.1

is a graphical representation of the stages of formation of the Danny Boy

crater.

Calculation of the true crater volume was accomplished by assuming

that its shape above the zero point was that of a rectangular hyperboloid

(Reference 3). Thus, confining the discussion for the moment to the upper

portion of the true crater, the equation of the crater wall can be repre­

·sented by

x2

~-c

where re represents the values of both the semitransverse and semiconju­

gate axes and x and y are horizontal and vertical coordinates,

1 v indicates last significant figure.

10

.,

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.,

. -· ,- r,, 1 ·

Page 23: UNCLASSIFIED AD NUMBER: AD0476502

. ~ : 1j' .• .. ,, :

respectively. The volume of the upper portion of the true crater can be

cetermined by considering the entire crater from original ground surface

to the depth of burst. (DOB or Z) to be inclosed within a right circular

cylinder of radius equal to the true crater radius (rt), and then sub­

tracting the volume generated by rotation of the area under the true crater

side (see Figure B.3.2a). Thus, with the volume of the lower portion of the

cavity added, an equation for the true crater volume can be written as

follows:

vt = volume of cylinder - volume under hyperbola+ volume of lower portion of cavity

(B.3.7)

This reduces to

Vt= 4.030 X 106 - 2.205 X 106 + 9.725 X 104

= 1.922 X 106

ft3

or 71,200 cubic yards. As will be noted in Figure B.3.2a, this procedure V

probe.bly results in a sanewhat lesser volume than that of the assumed

hyperbola and hence in a vt larger than the actual. \

B,3,4 ~TED MATERIAL

From Equation B.3.1, the volume of in situ rock dissociated by the

explosion is

The variables v f and vu are interchangeable in a soil medium but

apparently unrelated in canpetent rock. Because of the physical properties

of rock, it seems clear that vf did not contribute to the Danny Boy crater

formation. Since flowage did not occur, the upthru,st was apparently the

11

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Page 24: UNCLASSIFIED AD NUMBER: AD0476502

..... , ,·:

result of spallation in general and bulking of the material immediately

surrounding the crater rim. TheGe effects were attributed to the action

of the compressive shock wave and its r efl ection at ground surface and

to cas expansion in the cavity. Any volume initially formed by compression

in the upward direction is later neeated by ventine , so it is concluded,

at least for practical purposes, that the energy expended to form the

upthrust region actually made no contribution to crater size. It seems

likely that the same mechanism may occur to ::; ome extent in a deep burst

in soil.

Using the quantities previously developed,

vd. = 71,200 - (3, 610 + 0 + 12) = 67,578 yd3 is v

Either the dissociated mat2rial was ejected completely from the crater

to form the ejecta portion of the lip and the dust cloud, or it fell back

into the true crater to form the apparent crater. From Equation B. 3 .2,

The ratio

Therefore,

(Po) . Ve + V fb = ~ V dis

is approximately 4,250 lb/yd3 + 3,620 lb/yd3, or 1.17.

The volwne of the apparent crater, as determined by plan:imetric

measurement, was found to be 38,200 cubic yards. From Equation B,3,3, V

·· 71,200 - 38,200 = 33,000 yd3 V

Therefore,

= 79,000 - 33,000 = 46,000 yd3 V

12

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\--:~ " 'l',lo7 .• 'I :,: •!f,-,!:'!,i "-1.' ,,.<-;.IJ • .r , • J,W, ~ '~ ' ., } ' ',' • ~ ' ' •\.,, ~, ' ~r' ' ~ ., 1, , ' " • , • •

Page 25: UNCLASSIFIED AD NUMBER: AD0476502

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The compaction which initially occurs in the material above the cavity

(prior to ventinr, ) is not taken into account in thc~c equations . The

comminut ion which ac.:compani c!S venting probalJl y ncf~ates most of th r: initial

density chanl~<-~.

In the dust cloud formed by the explosion, particl es which wer e

essentially windborne we:rc transported far from GZ. From a careful esti.rlate

of the mass of the Sedan dust cloud (a nuclear event near optimum depth

in desert alluvium), it was concluded that in that event approximately

1 percent of the apparent crater mass was thus deposited beyond about 20

crater radii from GZ (Refer ence 8). Although the Danny Boy Project 1. 6

layout extended much farther than this, the deposition from the cloud could

not, at the greater distances, be distinguished by weight or volume from

dust accumulations from other sources. Observation of the event, however,

indicates that the scaled ejecta volume attributable to the dust 1 :loud was

much smaller than that of Sedan, which should be expected from a consider­

ation of the differences in the cratered media. As a rough estimate,

probably less than 0.5 percent of the apparent crater volume, or about

150 cubic yards of earth material, was in the Danny Boy cloud. V

With the completion of the crater lip in-✓estigations, direct measure­

ment of the ejecta volume is possible. Using the profiles of Figure B.2.3

and mathematically rotating geometric sections about the GZ axis, volumes

of the lip and upthrust regions can be computed. Thus, vJ, = 7~,800 cubic

yards and v = 20,500 cubic yards. The volume of ejecta in the lip U V

equals vi, - v , or 58,300 cubic yards. To this must be added the volume U V

of ejecta deposited beyond the lip but within the general crater area and

that transported far .away by the dust cloud. To find the fonner, a new

13

a

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-

. - - - - - - - ---------~---

Page 26: UNCLASSIFIED AD NUMBER: AD0476502

,,. ,, .,

mass distribution equation was computed by the meth:>d of l eact squares ,

us ine; only collec t or rings C, D, and E (440 to 880 f eet from GZ). Ring B

(310 fe et from GZ) was excluded because the :., tations on t.his ring which were

not recuvered wer e actually under the outer ede;e of the lip, and the results

f th ld t . ( s::_ 2 91 · 1018 R-S .S5) th . . d Th o . e o equa ~on u = • u X were us biase . e new

equation is

(B.3.8)

Where: 5 = mass distribution in kg/meter2 2

R = radial distance from GZ in met ~rs

The metric system is used here to perrnit direct comparison wi.th the equa­

tion for rings B through E develo_pPd in the main report to which this is an

appendiY.. Using Equation B.3.8 e..nd integrating from the outer edge of

the average crater lip to infinity,

CD

Ew = 2,r J 6 R dR 3

67 m

(B.3.9)

where Ew equals total weight of ejecta deposited beyond crater lip but

within general crater area. The concept of this integration and revolution

is shown graphically in Figure B-3.2b. Substituting,

a,

\, = 2n f (1.42 X 1019

R-8 ·86) R dR = 3,86 x 106 kg

"'67

2 Multiply kg/meter2 by 0.205 to obtain lb/feet2•

3 Multiply meters by 3.28 to obtain feet.

4 Multiply kilograms by 2.205 to obtain pounds (weight).

14

4

I . '

Page 27: UNCLASSIFIED AD NUMBER: AD0476502

w.· .. ) .

6 or 8.52 X 10 pounds. Using t,he postshot density given on page 3, this

weight is found to represent a volume of 2,360 cubic yards. Thus, by V

direct measurement, the entire volume of ejected material -- lip, close­

in deposit, and windborne -- is 61,000 cubic yards, to the greatest

accuracy justified by the input data. A logarithmic plot of mass dis­

tribution versus radial distance f1 ·om GZ for Danny Boy, revised to include

data points computed for the crater lip, is contained in Figure B.3.3.

The Sedan event, similar in. geometry but much larger in yield and in

a different medium, is included for comparison. Danny Boy crater vol­

umes are recapitulaterJ, to the greatest justifiable accuracy, in

Table B.3.1.

The discrepancy between directly measured and inferred ejecta volumes

( ... 15 ,000 cubic yards) represents the uncertainty of these measurementa

and/or inferences. The most likely sources of error are the true crater

volume and the density factor, p0/p1 . Subsurface exploration of the

true crater has been necessarily limited, and a considerable uncertainty

exists as to its size; also, the assumption of a hyperboloid configuration

results in an error (Section B.3.3). While the density factor appears to

be based upon a good sample (al.mat 1 percent of the total ejecta volume),

its value is suspiciously low. Errors in either true crater volume or the

density factor would tend to discred~t the inferred method, so the volume

of ejecta listed in Table B.3.1 is the direct measurement rounded off to

the nearest 10,000 cubic yarda. Division of the accumulated ejecta and

fallback volumes by vdis yields a density factor of approximately 1.3~,

which may more nearly represent the true density factor P0/P1 •

•. , , . . . . . ( ~ .: . . ' ,"

'-:· .: . •"

' . ' I .

15

.,,·

Page 28: UNCLASSIFIED AD NUMBER: AD0476502

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·,·,.

B.3.5 CORRELATION WITH PREVIOUS EXPERIMENTS

Using the foregoing computations, Figure B.3.2, and data from the

main text of this report (PORjwT-1815) a plot of ejecta deposition versus

distance from GZ has been prepared and is presented in Figure B.3.4. For

comparison, an envelope of data for shots in desert alluvium (from Refer­

ence 9) has been included. The envelope includes shot geometries from

near-surface to near-optimum DO~'s. Figure B.3.5 {from Reference 6) is a

plot of apparent crater volume versus total volume of ejecta for a similar

range of shot geometries in alluvium, to which the Danny Boy data have

been added. The upper and layer 1imits of these data were established by

the direct and inferred ejecta measurements, respectively.

16

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TABLE B.3.1 DIMENSIONS AND VOLUMES OF DANNY BOY CRATER REGIONS

Metric equivalents: 1 foot= 0.305 meters 1 cubic yard= 0.765 cubic meters

Crater Region Depth Average Volume or Radial Extent

Height from GZ Axis

feet feet cubic yards

Apparent crater 62a 108 38,000

True crater 146a 108 71,000

Fallback 84a 100 33,000

Lip (total) 25b 310 79,000

Lip (ejecta) llb 310 58,000

Lip (upthrust) 14b 220 21,000

Ejecta (total) 60,000

Crater cavity 36c 36 3,600

Dissociated material -- 68,000

Melted material 8d 75

Vaporized material 4d 12

a Below OZ. b Average maximum height above original ground surface. c Below zero point. d Ignoring device configuration (i.e. assuming true point source of

energy).

17

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Page 35: UNCLASSIFIED AD NUMBER: AD0476502

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B.4.1 CONCWSIONS

CHAPI'ER B.4

CONCLUSIONS A.ND RECOMMENDATIONS

A large difference is observed between direct and inferred measure­

ments of ejected material for the Danny Boy crater. An examination of the

various crater volumes reveals that:

1. The al):parent crater volume amounts to slightly more than half of

the true crater volume.

2. Approximately 65 percent of the material dissociated by the ex­

plosion, representing a volume about 1.6 times that of the apparent crater,

was permanently ejected from the crater; the remainder fell back within

the confines of the true crater. Thus, a significantly larger percentage

of ejecta was realized on this event than in similar shots in dry soil.

3. Ejecta accounted for almost three-fourths of the crater lip

volume; upthrust of the original ground surface was responsible for the

remainder.

4. More than 98 percent of the ejected material fell within 3

crater radii of GZ to form the lip. Distribution of ejecta was generally

much closer to GZ than for shots in dry soil.

B.4.2 RF£0MMEIIDATIONS

For tuture cratering experiments, it is recamnended that preshot plans

and preparations include an experimental array and measurement techniques

that will facilitate quantitative &n&l.ysis of the crater formation in terms

of the contributions provided by each cratering mechanism.

23

Page 36: UNCLASSIFIED AD NUMBER: AD0476502

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·- .. -----~------------------------------------......... ,... .......

REFERENCES

1. J. A. Miskel and N. A. Bonner; "Danny Bey: Distribution of the

Radioactivity fran a Nuclear Cratering Experiment"; Project 21.1,

WT-1817, 31 December 1964; University of California, Lawrence

Radiation Laboratory, Livermore, California; Unclassified.

2. N. M. Short; "Project Danny Boy: The Definition of True Crater

Dimensions by Post-Shot Drilling"; WT-1834, 6 July 1964; University

of California, Lawrence Radiation Laboratory, Livennore, California;

Unclassified.

3. J. F. Leisek; "Postshot Geologic Investigations of the · Danny Boy

Nuclear Cratering Experiment in Basalt"; UCRL-7803, 13 March 1964;

University of California, Lawrence Radiation Laboratory, Livennore,

California; Unclassified.

4. D. C. Banks and R. T. Saucier; "Engineering Geology of Buckboard

Mesa"; Atomic Energy Commission Preliminary Report PNE 5001P, July

1964; U. S. Army Engineer Waterways Experiment Station, Vicksburg,

Mississippi; Unclassified.

5. M. D. Nor~ke; "Project Danny Boy: Crater Studies"; ITR-1816,

15 Nov•ber 1962; University of California, Lawrence Radiation

Laboratory, Livermore, California; Unclassified.

24

\

. . ·\, , ,, I .... .,!.l_, : • \ '...,:·- ,- -.•-~-----------~

,; r ,! -~ .\. •

. \ --~' . \ ·. '\;

·. ·:. ~

,t· ' .•t

Page 37: UNCLASSIFIED AD NUMBER: AD0476502

,I

'';.-' • !--~~

' :_,;-?/'.::/~.- '\•

7. G. W. Johnson, G. H. Higgins, and C. E. Violet; "Underground Nuclear

Detonations"; UCRL-5626, 8 July 1959; University of California,

Lawrence Radiation Laboratory, Liver1nore, California; Unclassifi~d.

8. R. H. Carlson and W. A. Roberts; "Pl·oject Sedan: Mass Distribution

and Throwout Studies"; PNE 217F, 6 Angust 1963; The Boeing Company,

Seattle, Washington; Unclassified.

9. R. H. Carls~n an<i W. A. Roberts; "Distribution o:f.' Ejecta from Cratering

Explosions"; April 1963; The Boeing Company, Seattle, Washington;

Unclassified (Unpublished paper).

25

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I ! I

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Page 38: UNCLASSIFIED AD NUMBER: AD0476502

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DISTRIBUTION LIST

Ad.dress

Commanding General, Aberdeen Proving Ground ATTN: Director, Ballistic Research Laboratories Aberdeen, Md.

Commanding General, Army Materiel Command ATTN: AMCRD-DE-N, DA Washington, D. C.

Chief of Engineers, DA ATTN: ENGTE-P

ENG~-M ENGMC-DE ENGTE-E ENGCW-Z ENGAS-L ENGMC-M (Col. Bruce Jones)

Washington, D. c.

Director, U. s. Army Engineer Nuclear Cratering Group Lawrence Radiation Laboratory P. o. Box 808 Livermore, Calif.

Director, U.S. Army Cold Regions Research and Engineering Laboratory, ATTN: Mr. K. :Boyd

P.O. Box 282, Hanover, N. H.

Commanding General, U. S. Continental Army Command Ft. Monroe, Va.

Division Engineers, U.S. Army Engineer Divisions Continental United States (copy to each)

Camnanding General, The Engineer Center ATTN: Asst. Comma.ndant, Engineer School Ft. Belvoir, Va.

Commanding Officer, Engineer Research & Developnent Laboratories

ATTN: Technical Documents Section Ft. Belvoir, Va.

Chief of Research & Development, DA ATTN: Atomic Division Washington, D. c.

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No. of Copies

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Page 39: UNCLASSIFIED AD NUMBER: AD0476502

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Address

Air Force

Commander, AF Weapons Laboratory, ATTN: Capt. Harry Auld Kirtland AFB, N. Mex.

Director of Plans , Headquarters , USAF ATTN: War Plans Division Washington, D. c.

Director of Research & Development, Headquarters, USAF ATTN: Combat Components Division Washington, D. c.

Commander-in-Chief, Strategic Air Comm81ld ATTN: OAWS Offutt AFB, Nebr.

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Chief, Bureau of Ships, Dept. of the Navy ATTN: Code 423 Washington, D. c.

Chief, Bureau of Yards & Docks, DN ATTN: D-400 Washington, D. c.

Commanding Officer & Director, David Taylor Model Basin A'l'"ffl: Li bra.ry Washington, D. c.

Officer-in-Charge, U.S. Naval Civil Engineering Laboratory ATTN: Code 753 Port Hueneme, Calif.

Commanding Officer, U. S. Naval Damage Control Training Center, Naval Base, ATTN: ABC Defense Course

Philadelphia, Pa.

Director, U. S. Naval Research Laboratory Washington, D. c.

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Page 40: UNCLASSIFIED AD NUMBER: AD0476502

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Address

other DOD Agencies

U.S. Coast & Geodetic Survey ATTN: W. K. Cloud San Francisco, Calif.

U.S. Coast & Geodetic Survey ATTN: D.S. Gardner Washington, D. c.

Assistant Secretary of Defense (Research & Engineering) ATTN: Tech Library Washington, D. c.

others

Chairman, Armed Services Explosives Safety Board Room 2075, Bldg. T-7, Gravelly Point

Washington,~. c.

The Boeing Company P.O. Box 3707 (For M. V. Anthony) Seattle, Wash.

The Boeing Company (For R.H. Carlson) Albuquerque, N. Mex.

Director, Defense Atomic Support Agency Washington, D. c.

Director, Defense Atomic Support ATTN: Mr. John G. Lewis Washington, D. c.

Defense Documentation Center for Scientific and Technical Information,

Cameron Station, Va.

Mr. W.R. Perrett, 5112 Sandia Corporation, Sandia. Base Albuquerque, N. Mex.

Prof. F. E. Richart, Jr., Dept. of Civil Engineers University of Michigan

Ann Arbor, Mich.

The Sandia Corp. , Sandia Base ATTN: Classified Document Division (For M. L. Merrit,

Div. 5412; B. F. Murphey; L. J. Vortma.n; T. J. Fl~an) Albuquerque, N. Mex.

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Page 41: UNCLASSIFIED AD NUMBER: AD0476502

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Address

Dr. T. H. Schiffman, Illinois Institute of Technology 10 West 35th Street

Chicago, Ill.

'l'he University of Illinois, Civil Engineering Room 207, Talbot Laboratory, (For Dr. N. M. Newmark)

Urbana, Ill.

Director, Weapons Test Division, Sandia Corp., Sandia Base Albuquerque, N. Mex .

Prof. R. V. Whitman, Dept. of Civil Engineering Massachusetts Institute of Technology

Cambridge, Mass.

Suffield Experimental Station Ralston, Alberta, Canada

4

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