NASA Contr Report 3918 ai s c 3 

ctor

Design and Testing of an

Energy-Absorbing Crewseat

for the F/FB-111 Aircraft

Volume IIImData From Seat Testing

S. Joseph Shane " " : ' .... "'_'_......

CONTRACT NAS1-17387

AUGUST 1985

NASA Contractor Report 3918

Design and Testing of an

Energy-Absorbing Crewseat

for the F/FB-111 Aircraft

Volume IIImData From Seat Testing

S. Joseph Shane

Simula Inc.

Phoenix, Arizona

Prepared for

Langley Research Center

under Contract NAS1-17387

N/

Nationa

 A

l Aeronautics

and Space Administration

Scientificand Technical

Information Branch

1985

TABLEOF CONTENTS

Page

1.0 INTRODUCTION.......................... 1

2.0 NASATEST NO. 1......................... 3

3.0 NASATEST NO. 2......................... 19

4.0 NASATEST NO. 3......................... 38

5.0 NASATEST NO. 4......................... 56

6.0 NASATEST NO. 5......................... 74

7.0 NASATEST NO. 6......................... 93

8.0 NASATEST NO. 7......................... Iii

9.0 NASATEST NO. 8......................... 132

I0.0 NASATEST NO. 9......................... 152

11.0 NASATEST NO. 10 ........................ 172

12.0 NASATEST NO. Ii ........................ 193

13.0 NASATEST NO. 12 ........................ 214

14.0 NASA(IBAHRS) TEST NO. 17.................... 234

1.0 INTRODUCTION

This volume presents data from the testing of an energy-absorbing crewseat in

an F/FB-III crew module. A complete description of the program is contained

in Volume I: Final Report. Data from the dynamic test series on the seat is

contained in Volume II.

Dynamic testing of the energy-absorbingseat and the operationalF/FB-111seat

in an F/FB-111crew module was conductedat NASA Langley ResearchCenter. The

testing is describedin Section 4.0 of Volume I, and the resultingdata are presented in Sections 2.0 through 14.0 of this volume.

Table 1 lists the data recorded. The four axes recordedon the seat pan include

a measurementalong the seat back tangent line as well as the three major axes.

The seat deflectionwas measureda]ong the seat back tangent line, but the dynamic responseof the linearstring potentiometerscould not accuratelyshow

the seat stroke. Final seat strokewas measured and is recorded in Volume I.

DRI is presentedusing the same three accelerationmeasurementsused in the

seat testing: seat pan z-axis, seat pan along the back tangent line, and dummy pelvis z-axis.

The test conditionsare listed at the beginningof each chapter. To be positive, the sign conventionfor the crew module orientationis for the following

earth referenceconditions:

• Pitch - nose up

• Roll - right wing down

• Yaw - nose right.
TABLE 1. RECORDEDATAFROI4CRE_VMODULETESTING

Description of Data

(Number of Channels) Filter Class*

Accel erati on

Left Bulkhead (3) Class 60

Right Bulkhead (3) Class 60

Left Seat Pan (4) Class 180

Capsule Center of Gravity (C.G.) Class 60

Left DummyPelvis Class 180

Right DummyPelvis Class 180

Right DummyChest Class 180

Left DummyHead 666 Hz

Right DummyHead 666 Hz

Forces

Left Seat Pan (3) Class 60

Right Seat Pan (3) Class 60

Exit Port Pressures (6) Class 60

Seat Deflection (2) Class 60

Dynamic Response Index (3)

* Class 60 and Class 180 filters per SAE Recommended

Practice J211b.

2
2.0 NASATEST NO. 1

HORIZONTALVELOCITY: 34 ft/sec

VERTICALVELOCITY: 32 ft/sec

CREWMODULEPITCH: - 13o

CREWMODULEROLL: 0°

CREWMODULEYAW: 45o

LEFT SEAT: Energy Absorbing

RIGHTSEAT: Energy Absorbing

3
m

5-

0 _ ---1_ I I I I

× _-

-5 _----

-10 -

TIME (SEC)

LEFT BULKHEAD

NASA TEST NO. 1

4
lOI

X 5--

O- - I I I I

TIME (SEC}

RIGHT BULKHEAD

NASA TEST NO. 1
5-

X

-10 -

TIME (SEC)

LEFT SEAT PAN

NASA TEST NO. 1

6
5

y 0

Z -S 0

m 5-

W

o _ I I I I

o 0

c

-s _---

Z -

-10 _---

z

-20 --

IiiiiiiiiiIililllllllllllllllltlilllllllllllllllllllllllll

0 .0_ .08 .12 .16 .20

TIME (SEC)

RIGHT SEAT PAN

NASA TEST NO. 1

7
5

-5

Z -i0

-15

-20

-25

JillllillillilllllllllilIllllllllllilllilllilllillllllliil

0 .OU_ .08 .12 .16 .20

TIME (SEC)

CAPSULE C.G.

NASA TEST NO. 1

8
LEFT SEAT

2O

t5

tO

s

0 I I I I

Z

O

Itu RIGHT SEAT

- 20 I11

o

tO

,=: 15

10

5

0 I I I

-S

IIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIII

0 .OU= .08 .12 .16 .20

TIME (SEC)

SEAT PAN ALONG BACK TANGENT LINE

NASA TEST NO. 1
_

x O_ I ---T

TIME (SEC)

LEFT DUMMY PELVIS

NASA TEST NO. 1

10
5

X

0 I I

-5

TIME (SEC)

RIGHT DUMMY PELVIS

NASA TEST NO. 1

11
0 I I

x

-5

-10

TIME (SEC)

LEFT DUMMY CHEST

NASA TEST NO. 1

12
-5

z

-10

-15

-2O

-25

Iiiiiiiiillllllllllllllllllllllllllllllllllllllllllllllll

0 .OU_ .08 .12 .16 .20

TIME (SEC)

RIGHT DUMMY CHEST

NASA TEST NO. 1

13
LEFT DUMMY HEAD

NASA TEST NO. 1

14
sE0 I I I z"

x -5

-10

-15

RIGHT DUMMY HEAD

NASA TEST NO. 1

15
50--

LEFT SEAT

30-

'-' 10-

of

_ _."_k J-/ "---"

_,o

-3o- DR]=13.06

-_olllllllllll,,,),,,,)),,)l,,,,I,,,,)

•05 .10 .15 ._ ._ .30 .35

T ] l'l[

50--

RIGHT SEAT

30--

H 10--

no /.'-'\,

%",_,J/

-30- OR]:20.97

-50'''llllllll,,,I,,,,I,,,,Itllfl,lll!

•1_ .10 .15 ._ ._ .30 .35

T]ME

DYNAMIC RESPONSE INDEX

SEAT PAN Z-AXIS

NASA TEST NO. 1

16
m

so LEFT SEAT

30--

-- t \

o __! ',_,_,_J

_._i

-10

:,oL,,,,I,,,,I,,,,I,,,,I,,,, I,,,,I,,,,I

.05 •10 15 20 .25 :: iS

TIME

so RIGHT SEAT

DRI=22.68

-3[--

TIME

DYNAMIC RESPONSE INDEX

BACK TANGENT LINE

NASA TEST NO. 1

17
60--

LEFT SEAT

30--

'-' 10--

,o_ /i---..__/

I

IVI _'X i

/

-30-- DR]:23.37

•05 .10 .15 20 ._ .30 .35 TIME

50--

RIGHT SEAT

30-

'-' 10-

iv" ,,/-_

\ ,, P / ----

-_o- t _ : /

-39- DRI--23.92

-5o i t t i I t I i I I i i i i I i t i i I i i t t I i t i i I i t i t I

.o5 .lo .15 ._ ._ .3o ._5

TIME

DYNAMIC RESPONSE INDEX

DUMMY PELVIS Z-AXIS

NASA TEST NO. 1

18
3.0 NASATEST NO. 2

HORIZONTALVELOCITY: 34 ft/sec

VERTICALVELOCITY: 32 ft/sec

CREWMODULEPITCH: 0°

CREWr,iODULEROLL: 15o

CREWMODULEYAW: 90o

LEFT SEAT: Energy Absorbing

RIGHTSEAT: Energy Absorbing

19
5-

o L I _- I I I

x -

-5 _--

-10 -

k

15-

I0_ y -

£ oc 1- I I i

o -10 -

0

m

0 =_t-"-_ I I I I _ I

z -S _--

-10 _

Z

-15 --

0 .0_ .08 .12 .16 .20

TIME (SEC)

LEFT BULKHEAD

NASA TEST NO. 2

2O
m

10-

5_---

Y -50---_---- I.--- __ 0

"" -10 - Z

0

< 5- m /,.,

LI.I *

"LI,,I 0 __I I _1 _"_

O

O

< -5 --

-10 _---

-15 _---

D

z -

-20 _--

-25 _--

-30 _--

-35 m

0 .0_ .08 .12 .16 .20

TIME (SEe)

RIGHT BULKHEAD

NASA TEST NO. 2

21
10

5

x 0

-5

-10

5

Z

-10

-15

TIME (SEC)

LEFT SEAT PAN

NASA TEST NO. 2

22
10

5

x 0

-5

-10

15

10

5

- y CJ

-

Z 0

0

I-

< -5 a:

w

-J

w -10 ()

()

< 5

0

-5

-10 z

-15

-20

-25

-30 I1111II1I111111111111111111111111111111111111111111111I1I11I

o .04 .08 •12 . 16 .20

TIME (SEC)

RIGHT SEAT PAN

NASA TEST NO.2

23
-2O

IIIIIllllllllllllillllllllllllllllllllllllllllllllJlllll_ij

0 .Oli .08 .12 .16 .20

TIME (SEC)

CAPSULE C.G.

NASA TEST NO. 2

24
5-

0_ k I I I L___-_./-,

-5--

£ :

< -t0--

Z

J

W

o -15 _--

O

<

-20 _--

-25--

o .o_ .o_ .12 .l_ .2o

TIME (SEC)

CAPSULE C.G.

NASA TEST NO. 2

25
L_

25 LEFT SEAT

2O

15

10

5

o I I I

A -5

(9

Z

Om

ii.r

ILl

--I

uJ 30 - RIGHT SEAT tO

tO

< 25

2O

t5

10

5

o I I

-5

IIIIIIIIIIIIIIIIIlillllllllllillllllLlllllllllilllillfllllJ

0 .0L} .0B .12 .16 .20

TIME (SEO)

SEAT PAN ALONG BACK TANGENT LINE

NASA TEST NO. 2

26
TIME (SEC)

LEFT DUMMY PELVIS

NASA TEST NO. 2

27
-5

-lO

Z

-15

-2O

-25

-30

llllllllllllllllllllllllllllllillillllllllllllltlllllllll!ll

0 .04 .08 .12 .16 .20

TIME (SEC)

RIGHT DUMMY PELVIS

NASA TEST NO. 2

28
-25

iilll1111IllllllllllilllllllilillilliliIllililllillillIlii_

0 ,Oq ,08 ,1.2 ,16 ,20

TIME (SEC)

LEFT DUMMY CHEST

NASA TEST NO. 2

29
5

0 I I

-5

-I0

-_..0

Z

-15

-2O

-25

L.L_lllllllllllllllllJiiiiiiiilllllllllllllllllllllllllllllll

o .oq .o8 .12 .16 .2o

TIME (SEC)

RIGHT DUMMY CHEST

NASA TEST NO. 2

30
m

5--

/

0 __'.;= ..... L...... , .

X-5__

-tO --

-15 _

-2O --

5-

0 --_- - _4 I I I I

y -

-5 _---

_ -lO -

z 15-

£ _-

I_

111

--I

w 5

0

o

Z -

-tO _--

-t5 --

-20 --

-05 -

o .04 .o_ ._ ._6 .20

TIME (SEO)

LEFT DUMMY HEAD

NASA TEST NO. 2

31
- j

X -5

-I0

0

<a: -20

W

J

I.I.I

_..__,,._. r,._ J,,J._,.._I. i I • I

O_ .... .,,

-5

Y _

-IO

-15

lililillililllllliliiiliililllllllillliiliilllJiiiililliif

0 .0_ .08 •12 •16 .20

TIME (SEC)

RIGHT DUMMY HEAD

NASA TEST NO. 2

32
RIGHT DUMMY HEAD

NASA TEST NO. 2

33
SEAT STROKE

NASA TEST NO. 2

34
m

5O

LEFT SEAT

30--

'-' 10--

l / "----J

/

, }

DR]=_3.3L_

.05 .10 .15 .20 .25 .30 ._5

TIME

m

5O

RIGHT SEAT

3C--

.05 .I0 .15 .20 .N .30 ._5

TIME

DYNAMIC RESPONSE INDEX

SEAT PAN Z-AXIS

NASA TEST NO. 2

35
50--

LEFT SEAT

30--

'-' 10-- \

n,,

-10]''-"

-30- DR]--22.0_

50h

RIGHT SEAT

30-- ',I

-I0-- ""-'/

DRI=2q.6u_ -30--

-50'"'I''"I,,,,I,,,,I,,,,I,,,,I,,,,I

•= .Io .15 ._ .25 ._ ._5

TIME

DYNAMIC RESPONSE INDEX

BACK TANGENT LINE

NASA TEST NO. 2

36
5O

LEFT SEAT

30--

.."1o- //_\

\ \ / ' \_j"

-,o- \ , ,,

9 _---" DR]=2u,.16

-30--

-50 I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I

.05 .10 .IS .20 .25 .30 .35

T]ME

so RIGHT SEAT

30--

-50 I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I

•1_ .10 .15 20 ._ ._0 .35

T]ME

DYNAMIC RESPONSE INDEX

DUMMY PELVIS Z-AXIS

NASA TEST NO. 2

37
4.0 NASATEST NO. 3

HORIZONTALVELOCITY: 34 ft/sec

VERTICALVELOCITY: 32 ft/sec

CREWMODULEPITCH: 17o

CREWFiODULEROLL: 0°

CREWMODULEYAW: 90o

LEFT SEAT: Energy Absorbing

RIGHTSEAT: Energy Absorbing

38
X

LEFT BULKHEAD

NASA TEST NO. 8

39
10-

m

m

SR

x o_-_.... - I . __

z-lO

-15

-20

-25

-30

0 .04 .08 .12 .16 .20 .24

TIME (SEC)

RIGHT BULKHEAD

NASA TEST NO. 3

40
15

10

5

X 0

-5

-10

15

10

Y 5

LEFT SEAT PAN

NASA TEST NO. 8

41
10

0

x

-5

Z -10

RIGHT SEAT PAN

NASA TEST NO. 3

42
l0

5

x 0

-5

-I0

15

iO

-iO

Z

CAPSULE C.G.

NASA TEST NO. 3

43
Z 5 _- RIGHT SEAT

< 0 I I _A--•_-. f"-k

n- "_

LU

.J

I.U -5 0

0

-10

-15

-20

SEAT PAN ALONG BACK TANGENT LINE

NASA TEST NO. 3

44
10

x 0 I I

-5

-2O

IIIttl[Itlllllllltltltlttttlllllllltllltllllllllllltllll[llll

0 .0_ .08 .12 .16 .20 .24

TIME (BEG)

LEFT DUMMY PELVIS

NASA TEST NO. 3

45
10

5

x o I

RIGHT DUMMY PELVIS

NASA TEST NO. 3

46
10_

5--

x-5 _--

_10 _ \

t0--

"_ Y 5

z

£

0C....- J -- [

I.,I.I

o 5-- O

< 0- -_, -_. , I I ,;,/--i /

-IS --

20_

0 .0u, .08 .t2 .16 .20 .2_

TIME (SEO)

LEFT DUMMY CHEST

NASA TEST NO. 3

47
m

10-

m

5_---

X 0- I _ I ._ I

5

Y

0 I

-5

Z -10

IlllllllllIlllllllllIlllllllllIlllllllllJlllllllllJllllll

0 .0u_ .08 .12 .16 .20 .2Lt

TIME (SEC)

RIGHT DUMMY CHEST

NASA TEST NO. 3

48
Z

30--

,_

I.U

"J 25-- U.I

0

0

< 20 ----

Y 15---

-%, 1o--

5--

0 .0_ .08 .[2 .[6 .20 .24

TIME (SEO)

LEFT DUMMY HEAD

NASA TEST NO. 8

49
25--

20--

15--

10--

Z -

5

L_

o 0 I I

<

n-

!_1 -5

..I

LU

O

o -10

<

-15

-20

0 -0L_ .08 .i2 .16 .20 .2Li

TIME (SEC)

LEFT DUMMY HEAD

NASA TEST NO. 3

5O
10-

Y 5-

z

o

Iw 5

< O_

-5

Z

-10

-1S

-20 _

0 ,0_ ,08 ,12 .16 ,20 .2_

TIME (SEC)

RIGHT DUMMY HEAD

NASA TEST NO. 3

51
RIGHT SEAT

"7

5_--

Z

m

:

3_--

Z

z 2--

I--

z 1----"

ILl

ILl

o 0 I I I I

< m

Q. m

2 Z LEFT SEAT

1----

o_- I I I I !

0 .0u, .08 .12 .16 .20 .2u,

TIME (SEC)

SEAT STROKE

NASA TEST NO. 3

52
50

LEFT SEAT

30-

-30 DRI:20.'71

m

RIGHT SEAT

30--

'_ 10--

-10

DR]:22.tt8

-3_--

-50 I I I I I t I I I I I I I I I I I I I I

•1 .2 .3 J{

TIME

DYNAMIC RESPONSE INDEX

SEAT PAN Z-AXIS

NASA TEST NO. 3

53
50

LEFT SEAT

30--

-3o- DRI-18.66

•1 .2 .3 ._

TIME

5O

RIGHT SEAT

30--

'-' 10- f_

-10-- I /

/

/

-3o DRI =2[.62

.-5oI,,,I,,,,I,,,,I,,,,I,iifl,l,,I,,,,I

0 .05 .10 .15 .20 .25 .30 .35

TIME

DYNAMIC RESPONSE INDEX

BACK TANGENT LINE

NASA TEST NO. 3

54
m

so LEFT SEAT

30m

'-' 10--

-10

\

DR]:21.77

-30-

-50 I I I I ] I I I I ] I I I I I I I I I I

0 .1 .2 .3 .u=

"[]ME

m

5O

RIGHT SEAT

30--

_,o_ DRI -22 .t_u_

-30--

illtllllllllllllllll

0 .I .2 .9 .tt

T]ttE

DYNAMIC RESPONSE INDEX

DUMMY PELVIS Z-AXIS

NASA TEST NO. 3

55
5.0 NASATEST NO. 4

HORIZONTALVELOCITY: 34 ft/sec

VERTICALVELOCITY: 32 ft/sec

CREWMODULEPITCH: - 13o

CREWMODULEROLL: 0°

CREW_iODULEYAW: 75o

LEFT SEAT: Energy Absorbing

RIGHTSEAT: Energy Absorbing

56
w

5-

X -5

-10

-15 -

m

5-

Y 0 v.--_

m

z -SO m

<

n

w

O

< 0_ __

E

-5 _---

Z -I0 --

E

E

-15_---

-20 -

Ilillllltlllllllllllllllllllilillllllllilllllliilliillllll

0 .0_ .08 .12 .16 .20

TIME (SEC)

LEFT BULKHEAD

NASA TEST NO. 4

57
5-

o ._--------J _1 I _ ..-L_._. I

Z

x -5 --

Z

-10

-15 -

5-

Y 0- I _-_

Z

O 5--

0- -"q I I I

W --

o -5 _----

Z

-10 _

Z 2

-15_----

-20 _---

Z

-25 _---

-30 --

.l!llllllllllllllllllllllllllllllllj__jllllllll!lllll

0 .0q .08 .[2 .16 .20

TIME (SEO)

RIGHT BULKHEAD

NASA TEST NO. 4

58
x -B __--

-lO -

10 -

- • I

y 01_v-v - vz -5 --

0

P

<

W S--

Z

S_

Z

z-I0 _--

E

-15 _

E

-20 _--

-25 -

lilllililllliillillillllllllllllii,lililililll'lll

0 .0_ .08 .12 .16 .20

TIME (SEC)

LEFT SEAT PAN

NASA TEST NO. 4

59
0 .0u, .08 .12 .16 .20

TIME {SEC}

RIGHT SEAT PAN

NASA TEST NO.4

6O
0 I

X -5

-I0

Y 0 I

CAPSULE C.G.

NASA TEST NO. 4

61
5 LEFT SEAT

o I I

-5

-L0

-15

-2O

-25

0 .04 .08 • 12 • 16

TIME (SEC)

SEAT PAN ALONG BACK TANGENT LINE

NASA TEST NO. 4

62
LEFT DUMMY PELVIS

NASA TEST NO. 4

63
m

-25--

-30 -

Ilillllllllllllilil]lliiJllllllllilllllllillllllll

0 .0_ .08 .12 .16 .20

TIME (SEC)

RIGHT DUMMY PELVIS

NASA TEST NO. 4

64
LEFT DUMMY CHEST

NASA TEST NO. 4

65
Z

x -S _---

_-

-10 _---

-15 -

-25

0 "0L_ .08 .12 .16 .20

TIME (SEC)

RIGHT DUMMY CHEST

NASA TEST NO. 4

66
LEFT DUMMY HEAD

NASA TEST NO. 4

67
$

o I

X

-5

-10

SY 0 ........ "-+_r'

RIGHT DUMMY HEAD

NASA TEST NO. 4

68
SEAT STROKE

NASA TEST NO. 4

69
__ LEFT SEAT 6-

5--

u___

z

I-.

Z

:_ 2-- ILl

O

,:1:

,..I

n 1 --

o, I I I

o .o_ .o8 ._2 ._ ._o

TIME (SEC)

SEAT STROKE

NASA TEST NO. 4

7O
_o-- LEFT SEAT

301

'_ 10--

tY 11"-_

_ _ '_, / ,' _-/

40 _ _!,/i

40- DR]=20.52

,,,,I,,,,I,,,,I,,,,I,,,,I,,,,I,,,,I

•05 .10 .15 ._ ._ 30 45

I]ME

so-- RIGHT SEAT

304

-So , , , i I i i I i I i i i i I i i i i I i i i i I i i i i I i I i i I

0 ._ .10 .15 ._ ._ -_ ._5

T]ME

DYNAMIC RESPONSE INDEX

SEAT PAN Z-AXIS

NASA TEST NO. 4

71
50 --

LEFT SEAT

30--

'-' 10--

-30- DR:20 ] u.,7

-60'",ll,i,l,,i,l,,,_lii,,l,,,,l,,,,l

0 .05 .I0 .15 .20 .[5 ._0 .35

TIME

50--

RIGHT SEAT

30--

-,o /-\

-,o- _t tL 11

l#-._..

-3o DR]-21.92

-so'li'lili'liii,li,,,lili,liii,liilll .o5 .io .15 .2o ._ ._ .35

T ] I'IE

DYNAMIC RESPONSE INDEX

BACK TANGENT LINE

NASA TEST NO. 4

72
I

so LEFT SEAT

H I0-- \

If

, DRI=23.2tt

-30--

-50 I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I

0 .05 ,10 .15 .20 .25 .30 .35

TIME

n

5O

RIGHT SEAT

30--

D r \\

'_-\\ #'/ 11 .... _ /

o DRI=23.95

-30--

-5o,,,,l,,,,l,,,,llllilillil,,,,l,,,,l

0 .05 .I0 .15 .20 .L:X3 ._0 .35

TIME

DYNAMIC RESPONSE INDEX

DUMMY PELVIS Z-AXIS

NASA TEST NO. 4

73
6.0 NASATESTNO. 5

HORIZONTALVELOCITY: 34 ft/sec

VERTICALVELOCITY: 32 ft/sec

CREWMODULEPITCH: 17o

CREWMODULEROLL: 0°

CRE_MODULEYAW: 45o

LEFT SEAT: Energy Absorbing

RIGHTSEAT: Energy Absorbing

74
LEFT BULKHEAD

NASA TEST NO. 5

75
5-

X 0 - _ _ I _-,.-/'Ni A_/_ I I _ _

_ k.___ '-_

g---

_ o_-- I I I I _j

_ s---

_ -s;--

_ -10 --

-z -15

-30

-35 -

0 ,04 .OB •12 .16 .20 .2_

TIME (SEC)

RIGHT BULKHEAD

NASA TEST NO. 5

76
10-

TIME (SEC)

LEFT SEAT PAN

NASA TEST NO. 5

77
10

S

x 0

-5

-10

l''''II ,II,,,,IIIIIlIII ,,,,,l

0 .0Lt .08 .12 .16 .20 .2u

TIME (SEC)

RIGHT SEAT PAN

NASA TEST NO. 5

78
I0

5

x 0 I

-5

-10

-25

IIIIIlllllllllllllllllllllllllllilllllllllllllillllliilll

0 .0_ .08 .1.2 .16 .20

TIME (SEC)

CAPSULE C.G.

NASA TEST NO. 5

79
5

CAPSULE C.G.

NASA TEST NO. 5

80
SEAT PAN ALONG BACK TANGENT LINE

NASA TEST NO. 5

81
5

xo _Aj

-5

LEFT DUMMY PELVIS

NASA TEST NO. 5

82
I0

-5

Z -I0

-15

-20

-25

l,i,ii,,,,lIIIl,,I,,l ,li,lJl'l'I

0 .04 .08 .12 .16 .20 .2u,

TIME (BEG)

RIGHT DUMMY PELVIS

NASA TEST NO. 5

83
X

-5 --

I

-10 -

-5

Z

-10

-15

-2O

-25

o .o_ .08 .12 ._ ._o ._

TIME (SEC)

LEFT DUMMY CHEST

NASA TEST NO. 5

84
(.9

Z

0m

I.-

n-

_l - ] 1

y --

-t5

J

0 .0u, .08 • 12 • 16 .20 .2u,

TIME (SEC)

RIGHT DUMMY CHEST

NASA TEST NO. 5

85
RIGHT DUMMY CHEST

NASA TEST NO. 5

86
m

5-

- i I I I

0 '--"-:--_-'_47_-1;, .....;",--',-:'-'_

x -

-5 _---

-10 -

D

A

Z

w i0

<

W

,,, 5

0

° I < 0

Z-S

-10

-15

-20

ilillililliilllliJlllillllillllllJlilillilllliillllilllll

0 .OLI .OB .12 .16 .20

TIME (SEC)

LEFT DUMMY HEAD

NASA TEST NO. 5

87
i

x-5 !

-I0I

-- I .... I I I I I

Y-5

Z

-10 II

B

z 10

9

<

5

w

W

o

o 0

<

Z -5

-i0

-t5

-20

-25 I

0 .04 .08 ,12 .16 .20

TIME (SEO)

RIGHT DUMMY HEAD

NASA TEST NO. 5

88
D

m

tl __---" RIGHT SEAT

_

10---

9_--

8_--

'7_--

6_--

5_--

4_--

3_--

I'-

Z

uJ

LIJ

<

0., O__

co

5 ---" LEFT SEAT

Lt_----

3_----

2_----

1_

o- I I

IIIIIIIIIIIIIIIIIIlllllllllllllllllllllllllllllllllllllll

o .o_ .o8 .t2 .t6 .20

TIME (SEC)

SEAT STROKE

NASA TEST NO. 5

89
b

5o LEFT SEAT

30--

-,_0 I I I i I I i i I I I I I I I i I t I I i I I t I i I I I i I I I I I

0 .05 .IO .15 .20 ._5 .30 .35

TIME

so RIGHT SEAT

30--

;,o_rS:

,.

-10--

-3o-- DR]:22.89

-5o i i , ! I i t i t I i i l i I i t t i i i i l t I i t t t I i i i l I

.05 .tO .15 .20 25 .30 .35

TIME

DYNAMIC RESPONSE INDEX

SEAT PAN Z-AXIS

NASA TEST NO. 5

90
so-- LEFT SEAT

30--

H 10--

n,'

(3

-1o- _/_, , / I -

-30- DRI:21.51

-so,,111,,,11,,,11,,,11,,,11,,,11,,,11

0 .05 .10 .15 .20 .25 .30 .35

TIME

so-- RIGHT SEAT

30--

I / PL'I \

10-- _ •;/{ t \.

J A/ \ \ , f'-_

-io-- "-J

DR]=2_.5_

-30--

.-50 I I I I I i I I I I I I I I I I I i I I I I I I ! i i i i I i I i ! I

0 ,05 .10 .15 .20 ._ .SO .35

TIME

DYNAMIC RESPONSE INDEX

BACK TANGENT LINE

NASA TEST NO. 5

91
5o- LEFT SEAT

30 --

I_. / / \ \ /N / \

D _.,,_.J_// • \ .... '%,,,,X. /

I

-Io- \ /

xx,.j/

DR]--26.86

-30---

-_o______h_ ,_Lh,_,J__t-L_ L LL[_L[.LJ__..t. ILJ_l_UL_L]I._

•65 .I0 .15 ._ ._ .30 .)5

TIME

so- RIGHT SEAT

90--

-50 I I I I i I I I I I I I I I ] I I I I I I I I I I I I I i I i i i i I

0 .05 .10 .15 .20 ._ 30 .95

TIME

DYNAMIC RESPONSE INDEX

DUMMY PELVIS Z-AXIS

NASA TEST NO. 5

92
7.0 NASATEST NO. 6

HORIZONTALVELOCITY: 43 ft/sec

VERTICALVELOCITY: 32 ft/sec

CREWMODULEPITCH: 2o

CREWMODULEROLL: 0°

CREWMODULEYAW: 0°

LEFT SEAT: Energy ADsorbing

RIGHTSEAT: Energy Absorbing

93
TIME (SEC)

LEFT BULKHEAD

NASA TEST NO. 6

94
Y i0-52_____ _ O- I _Xx_ r_--/xJ I

zO -S-

--

I-"

tlJ

..j --

O --

< O_ B_ I I I

-5 --

Z

z-I0 --

-IS _

-20 _--

-25 -

o .m .oa .i:_ .16 .:m .au

TIME (SEC)

RIGHT BULKHEAD

NASA TEST NO. 6

95
5

-5

Z-t0

-15

-2O

IIIIIIIIIIIIIIIIIIIllIIIIIIIIilliiiiiiiiIiiiiiiiilliiiiiii

0 .04 .08 .12 .16 .20 .2_

TIME (SEO)

LEFT 8EAT PAN

NASA TEST NO. 6

96
m

10-

5 ZX - A I_^ I

0 __"_ v

10

Z

5

o I

IIIllll llllilllillllllllllllllllllllllllllllllllllllllllil II

0 .0LJ: .08 ..t2 .16 .20 .2£

TIME (SEC)

RIGHT SEAT PAN

NASA TEST NO. 6

97
0

CAPSULE C.G.

NASA TEST NO. 6

98
CAPSULE C.G.

NASA TEST NO. 6

99
20 LEFT SEAT

15

10

5

o I I 1

-5 ,,-J

z

0m

I-

<

nI.U

.,.I

LU

O

o 20

< RIGHT SEAT

15

10

5

_/_ _v,.,._, _ V. v I

-5

o .o_ .o8 .12 .!_ .2o .2_

TIME (SEC)

SEAT PAN ALONG BACK TANGENT LINE

NASA TEST NO. 6

100
[5-

[0

0 I I l

-5

35 A

Z

o 30 _--

w 25--

W

O

o 20 --

y

15 --

tO

5--

- I

0

0 .04 .08 .t2 .16 .2O .24

TIME (SEO)

LEFT DUMMY PELVIS

NASA TEST NO. 6

101
5

-20

I,,,,I,,,,I,,,,,lil,l,,,,,ll,,l,,l,,,,,,I,,,,,,,llllll,,,,jll

o .o, .o8 .12 ._ .2o ._

TIME (SEC)

LEFT DUMMY PELVIS

NASA TEST NO. 6

102
15

x 5

,5

IIJimJlllllllllllllJlllllllllllllllllll_ltlLliillllll'lllll_l

0 .0u, .08 .12 .16 .20 .24

TIME (SEC)

RIGHT DUMMY PELVIS

NASA TEST NO. 6

103
-25

lllllllIlllIIIllllllIlllillllIllllilllllllIllIiiIIIliIlllIIiI

0 .OU_ ,00 ,12 ._6 .20 .2_

TIME (SEC)

LEFT DUMMY CHEST

NASA TEST NO. 6

104
5

o I I

X

-5

RIGHT DUMMY CHEST

NASA TEST NO. 6

105
Y

0 ........ : _ I

LEFT DUMMY HEAD

NASA TEST NO. 6

106
m

B

30 m

25 _---

Z

20 m

Z

15 Z'-

z

10_--

× z

5

o I

-10

-15

-- I .______4_ _u_'_.:__'_

5-

I

-- Y o_ _-_.--

"

.......

........ +€-%_t,-%

z -8--

0

I-

._ -I0_---

n"

w 15 Z_

III Z

tO

O_ I0_---5___.Z_z_ _ &

Z -5 --

-IO Z--

-IS Z--

-20 _--

-25 -

0 .0'4 .08 •12 •16 .20 .2'4 .2B .32

TIME (SEC)

RIGHT DUMMY HEAD

NASA TEST NO. 6

107
so-- LEFT SEAT

301

I

-10

-3o DR]=2[.02

-so

0 .05 .I0 .15 .20 .25 ._0 .35

TIME

50--

RIGHT SEAT

30--

DYNAMIC RESPONSE INDEX

SEAT PAN Z-AXIS

NASA TEST NO. 6

108
so- LEFT SEAT

30--

'-' I[--

D

-10--

-3o- DR]=20.25

-._,,,,I,,,,I o ,l,,I,,,,I,,,,I,,,,I,,,,I

•05 .lO .15 .20 .25 .30 .35

T]ME

-30- DR]:21.B3

.-5o,,,,I,,,,I,,,,I,,,,I,,,,I,,_,lll,,l

0 .G5 .10 .15 .20 .25 .30 .35

i ] ME

DYNAMIC RESPONSE INDEX

BACK TANGENT LINE

NASA TEST NO. 6

109
SO--

LEFT SEAT

30--

-5of J n I I gn I I [ I I n ! J n I t ! I i i i i [ i i i i [ i i i i_

0 .05 .I0 .15 .20 ._ .30 ._5

TIME

so RIGHT SEAT

30--

-so nl nnn! n =lnn,jn n l,,t,l,,nnl

0 .05 .10 .15 .20 ._ .30 .35

TIME

DYNAMIC RESPONSE INDEX

DUMMY PELVIS Z-AXIS

NASA TEST NO. 6

110
8.0 NASATEST NO. 7

HORIZONTALVELOCITY: 43 ft/sec

VERTICALVELOCITY: 32 ft/sec

CREWf,_ODULEPITCH: 7o

CREWMODULEROLL: 0°

CREWHODULEYAW: 180o

LEFT SEAT: Energy Absorbing

RIGHTSEAT: Energy Absorbing

111
2O

15

× I0

0 I I --',, 

LEFT BULKHEAD

NASA TEST NO. 7

112
z y

0

V-. o I

i.r

w

..1

0 I I I

-5

Z

-10

-IS

o .o_ .o8 ._2 ._ .2o ._

TIME (SEC)

RIGHT BULKHEAD

NASA TEST NO. 7

113
15

10

X

5

o I I

I0

5

LEFT SEAT PAN

NASA TEST NO. 7

114
15

I0

x5 \

o I I I

y-sO_-- -,,,.,..,,, vvV? V--,

Z --

o

I--

<

,,, _-

.J

,,, S_----

< 8 ""_-'-'

-S _--

z -

-lO _----

-1S _---

-20 -

IIIIIllllllllllllllllllllllllllllllllllllllllllllllllllllllll

O .Ott .OB .12 .16 .20 .2q

TIME (SEC)

RIGHT SEAT PAN

NASA TEST NO. 7

115
CAPSULE C.G.

NASA TEST NO. 7

116
o- ! I

Z -5

-i0

-15

0 ,0_ .08 .t2 .16 .20 .24

TIME (SEC)

CAPSULE C.G.

NASA TEST NO. 7

117
LEFT SEAT 20 -

15

10

5

o I

-[0 -

z

O

<

m [0- RIGHT SEAT

W

O

o 5

<

'

5

-lO

-IS

-20 -

0 .0_ .08 .t2 .16 .20 .2_

TIME (SEC)

SEAT PAN ALONG BACK TANGENT LINE

NASA TEST NO..7

118
o I I I

Z

-S

-tO

-iS

llllllllllllllllllllIlllllllllllllllllllllllllllllIllllllllll

0 .04 .08 .12 .t6 .20 .24

TIME (SEC)

LEFT DUMMY PELVIS

NASA TEST NO. 7

119
RIGHT DUMMY PELVIS

NASA TEST NO. 7

120
LEFT DUMMY CHEST

NASA TEST NOo 7

121
5-

A

(9

Z

O

I,-

< 5 n,-

I.U

--I

14.1

o 0 I I I

O

-5

Z

-10

-15

-20

Iiiilllllllllllllllllllllllllllllllllllllllllllllllllllllllll

o .0_ .08 .12 .18 .20 .2_

TIME (SEG)

LEFT DUMMY CHEST

NASA TEST NO. 7

122
RIGHT DUMMY CHEST

NASA TEST NO. 7

123
35_

30_

\

25 _--

20 _--

x 15--

10--

-

o

- /

,_ --

n- --

W

-5 --

ILl

0

0

<

5-

E

0 _%_.... -__.... ___.:.-_,"'__,,, -'_--q_vl, -- -.... I

E

Y -5 --

E

-i0--

0 .0_ .08 ,12 ,16 .20 .2U

TIME (SEC)

LEFT DUMMY HEAD

NASA TEST NO. 7

124
LEFT DUMMY HEAD

NASA TEST NO. 7

125
RIGHT DUMMY HEAD

NASA TEST NO. 7

126
20-

.-, 15

z

_o I0

<

a: S w

.J

w

o

o 0

< Z

-S

-lO

-15

-20

-25 -

-jllllllllllllllllllllll,_,ll,lllllllllllllllll,llllllJlllhl I

0 ,0_I ,08 ,12 .iS .20 .24

TIME (SEC)

RIGHT DUMMY HEAD

NASA TEST NO. 7

127
SEAT STROKE

NASA TEST NO. 7

128
5o-- LEFT SEAT

30--

OR]:22.29

-30--

-50 I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I

0 .05 .10 .15 ._ .25 .30 .35

TIME

m

50 RIGHT SEAT

3_m

'-' 10--

,,y

-50, I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I ! I I I I

•05 .tO .15 ._0 25 .30 .35

TIME

DYNAMIC RESPONSE INDEX

SEAT PAN Z-AXIS

NASA TEST NO. 7

129
50--

LEFT SEAT

30--

'_ 10--

° _ 't__'___

50--

RIGHT SEAT

30--

I0- !r_ + !,,!Its+,

_,\\ / _' _/_t;),l)'I'l ,IY -_....

_,o-'_+A. ,]?+'

40-- •DRI=18.96

.so''''l''',lJ,llllllf11111111_lllllll

0 .05 .I0 .15 .20 .25 ._ .35

TIME

DYNAMIC RESPONSE INDEX

BACK TANGENT LINE

NASA TEST NO.. 7

130
m

5O

LEFT SEAT

H IO--

DRI=18.96

-30 -50I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I I

0 .[E .10 .15 .20 -_ 30 35

TIME

so RIGHT SEAT

30--

'-' 1(]--

o =----_\

-,o- \/_/

BE] -21.06

-30-

__,ll,,I,,,,I,,,,I,,,,I,,,,I,,,,I,,,'l

•05 .I0 .15 -_ .25 30 45

TIME

DYNAMIC RESPONSE INDEX

DUMMY PELVIS Z-AXIS

NASA TEST NO, 7

131
9.0 NASATEST NO. 8

HORIZONTALVELOCITY: 0 ft/sec

VERTICALVELOCITY: 32 ft/sec

CREWf,IODULEPITCH: 2o

CREWMODULEROLL: 0°

CREWMODULEYAW: 0°

LEFT SEAT: F-1110perationa|

RIGHTSEAT: Energy Absorbing

132
_

Y O- I I +,,-,, L _ I I _ _ I

Z

0

l--

ILl

,-I

ILl

0

0 5-

0_ , -_ , , _+_

L_..

-5 _--

Z -

-10 --

-15 --

-213-

o .o,+ .08 ._ ._6 .20 .a_

TIME (SEC)

LEFT BULKHEAD

NASA TEST NO. 8

133
5k

x o I I I v

-S

RIGHT BULKHEAD

NASA TEST NO. 8

134
LEFT SEAT PAN

NASA TEST NO. 8

135
RIGHT SEAT PAN

NASA TEST NO. 8

136
CAPSULE C.G.

NASA TEST NO. 8

137
SEAT PAN ALONG BACK TANGENT LINE

NASA TEST NO. 8

138
(9

Z

0

F-

<

tr

w

m 0 I _I I I .I

o __

0

< Z

-5 EZ

-10 Zz Z

-15 ---

Z

-20 _--

Z

-25 -

0 .0_ .OB .12 .16 .20 .2_

TIME (SEC)

LEFT DUMMY PELVIS

NASA TEST NO. 8

139
15-

iO C---

x 5_--

oZ- _ ..... '

RIGHT DUMMY PELVIS

NASA TEST NO. 8

140
m

5-

t_

Z

Oi

I--

,'," 0 i -_ J--_ I

__

.j --

-lO _--

z-15

-20 _---

-25 _----

-30 -

,,,,,,,,,l,i,,,Ji,,l,,,,,,,,,lili,,,,,,i,,,,,,,,,l,,,,,,,,l I

0 ,04 .08 .12 .16 .20 .24

TIME (SEC)

LEFT DUMMY CHEST

NASA TEST NO. 8

141
RIGHT DUMMY CHEST

NASA TEST NO. 8

142
v

2 5-

I--

oc 0

ILl

IJJ

0

o -S _---

-tO _-

Z

-iS _--

-20 _--

-25_--

-30-

0 .0Lt .08 .12 .t6 .20 -2Lt

TIME (SEC)

LEFT DUMMY HEAD

NASA TEST NO. 8

143
B

O-- I ._.,

x -5 --

RIGHT DUMMY HEAD

NASA TEST NO. 8

144
LEFT THIGH

_00-

J

200-- W

0

Z

o 0 I I i

o .o_ .08 .12 ._6 .20 ._

TIME (SEC)

LEFT SEAT PAN LOADS

NASA TEST NO. 8

145
CENTER

2600 -

2400

2200 --

2000 --

[800--

1600--

1400--

1200 --

m

i000--

W

0

o 800--

600--

_00 --

200--

O- I I I I

RIGHT THIGH

-200

IllillllllllllllllllllllllllllillllllltillltllilllIlilllllliI

0 .0_ .08 .12 .16 .20 .24

TIME (SEC)

LEFT SEAT PAN LOADS

NASA TEST NO. 8

146
LEFT THIGH

_00-

2O0 ZZ

o- I I I

CENTER

[600

lqO0 --

1200--

[O00--

J

m 800 --

0

0

600--

_00--

200 --

: ] ] 1 l ---J 0

RIGHT THIGH

0 I _ I I

0 .0_ .08 .12 .t6 .20 .2_

TIME (SEC)

RIGHT SEAT PAN LOADS

NASA TEST NO. 8

147
RIGHT SEAT STROKE

NASA TEST NO. 8

148
•_o-- LEFT SEAT

30--

'-'I0-- _v / _, \

-10--

DR]=23.91

-30--

-5o--u--uI,,,, I ,,,, I,, ,, I,,,, I,,,, I, , i , I

0 .05 .IO .15 .20 .25 ._ 45

TIME

m

50

RIGHT SEAT

30--

_'V/_ \ \\\ H IO-- ¢

.2y/

-I0 --

4D- DR]-18.69

-._o,,,,I,,,,l,,,,l,,,,I,,,,I_,_,,, I,,I

O .05 .10 .15 .20 ._ .30 .35

TIMF

DYNAMIC RESPONSE INDEX

SEAT PAN Z-AXIS

NASA TEST NO. 8

149
50-- LEFT SEAT

30--

I0- ;L/ _, \\\

,_J/ % \

\. \ F" /

-lO--

DR]=22.83

-30--

-50 I I I I I I I I I I I I I I I I I I I I I I I I II I I I I I I I I I

.05 .10 .15 .20 .25 30 .35

TIME

B

5o

RIGHT SEAT

30--

1o- K "\\

\ / '

-10--

DRI-23.65

-30--

-50 I I I I I I I I I I I I I I I I I I I I I I I I I I I I i I i i i i I

•05 .tO .15 .20 -25 30 .35

TIME

DYNAMIc RESPONSE INDEX

BAcK TANGENT LINE

NASA TEST NO. 8

150
50--

LEFT SEAT

30--

'_ 10--

rr" f-_,

, \

-10--

/

0R]:2Lt.58

-38--

•05 .10 .15 20 .'25 30 45

TIME

50

RIGHT SEAT

30--

-50 I I I t t I I I I I i I t t I I I I I I I I I I t I I I I I t I I I I

0 ,05 .I0 .15 ,_ .E5 30 .35

TIME

DYNAMIC RESPONSE INDEX

DUMMY PELVIS Z-AXIS

NASA TEST NO. 8

151
10.0 NASATEST NO. 9

HORIZONTALVELOCITY: 0 ft/sec

VERTICALVELOCITY: 25 ft/sec

CREWMODULEPITCH: 2o

CREWMODULEROLL: 0°

CREWMODULEYAW: 0°

LEFT SEAT: F-Ill Operational

RIGHTSEAT: Energy Absorbing

152
x 0- I I _l -- I ._I _ i

S __

o I"-,, I I I I I

Z-5 --

,10

•15 -

0 .0LL .08 .12 .16 .20 .2u_

TIME (SEC)

LEFT BULKHEAD

NASA TEST NO. 9

153
I

5-

I

Y O_ I I _ _--f--- I I ""-v j z - _

w

.J

W

o

5-

O- _ I I I I I

-5 _--

z

-1On

lllllllllllllllllllIiillllllllllllllllllllllllllllllllllllll

0 .04 .08 .t2 .16 .20 .24

TIME (SEC)

RIGHT BULKHEAD

NASA TEST NO. 9

154
m

5-

(.9

--5 B Z

Oi

I-

,_.

LIJ

,..I

LLI

O

O

15

10

Z 5

0 I I I k/_

-5

0 .0u, .08 .12 .].6 .20 .2u,

TIME (SEC)

LEFT SEAT PAN

NASA TEST NO. 9

155
RIGHT SEAT PAN

NASA TEST NO. 9

156
5-

y O- I _IvA _.__.-I----_vA IJ_ /"X.I I

_ v _ __ /,.--'-'_ _,,

V -

Z

0

Ii-1-

iii

-I

IIi

SO %-, I I I I 1

z-5 __--

-I0 _-

-15 -

CAPSULE C.G.

NASA TEST NO. 9

157
SEAT PAN ALONG BACK TANGENT LINE

NASA TEST NO. 9

158
TIME (SEC)

LEFT DUMMY PELVIS

NASA TEST NO. 9

159
10

5

X

0 I

-5

-2O

liillllllillilllJltlllillilllilillillilllllllllllllllllilllll

0 .O4 .08 .12 .].6 .20 .2_

TIME (SEC)

RIGHT DUMMY PELVIS

NASA TEST NO. 9

160
TIME (SEC)

LEFT DUMMY CHEST

NASA TEST NO. 9

161
RIGHT DUMMY CHEST

NASA TEST NO. 9

162
5-

-5

-10

5

£ -5

I--

tr

UJ

-' 5 LLI

0

< 0 _

-5

z

-10

-15

-20 -

[,,,,,,,,,l,,,,,,,,,I,,,,,,,,,I,,,,,,,,,l,,,,,,,,,I,,,,,,,,,I

0 .OLt .08 • 12 • 16 .20 .2_

TIME (SEC)

LEFT DUMMY HEAD

NASA TEST NO. 9

163
D

Y 0 _.-;......:.:, I, .. . ..l_._.._.'..,',__..,,r_._*'_'__M__.;_,_

z -SO

IIJJ

-.I

I.kl

0

o 5----

-S

z

-10

-15

-20 -

,,,,,,,,,l,,l,,,,,,l,,,,,,,l,i,,,,,jl,,l,,,,l,,,,I,,,,,,,,,l o .o_ .o_ ._2 ._ .20 .2_

TIME (SEC)

RIGHT DUMMY HEAD

NASA TEST NO. 9

164
LEFT SEAT PAN LOADS

NASA TEST NO. 9

165
LEFT THIGH

200 -

o- I I I I I I

-200 -

A

m-I RIGHT THIGH

o'" ttO0 _-- _

nO 200 --

II

m

-200 -

0 .04 .08 .12 .16 .20 .24

TIME (SEC)

RIGHT SEAT PAN LOADS

NASA TEST NO. 9

166
m

200 -

_ 0 - I I I I I I

_ _

mW -200 -_

0 .04 ,08 .12 .16 .20 .24

TIME (SEC)

LEFT REAR EXIT PORT PRESSURE

NASA TEST NO. 9

167
__ RIGHT FRONT

200 -

0- I I I I I I

-200 -

__ RIGHT CENTER 200 -

i

o. 0 I I I I I I

m -200 -

(/)

1.1.1

no.

RIGHT REAR

200 -

0- I I I I I I

-200 -

0 .0u, .08 .12 .t6 .20 .2u_

TIME (SEC}

EXIT PORT PRESSURES

NASA TEST NO. 9

168
m

so LEFT SEAT

30--

-ll_--

-30- DRI-lq.6q

,,,,I,,,,t,,,,I,,,,t,,,,I,,,,I,,,,I

.05 .tO .15 .20 ._ .30 .35

TIME

B

5O

RIGHT SEAT

30--

'-" 10- ..,Jr"K "\,. _ ,..---.,..

o =__,_._..__ . ., -"<5 / -'"'%'_-'-

-I_--

-30--

DRI:1q.26

-so,,,,I,,,,I,,,,I,,,,I,,,,11,,,I,,,,I

0 .05 .10 .15 .20 ._ .90 .35

TIME

DYNAMIC RESPONSE INDEX

SEAT PAN Z-AXIS

NASA TEST NO. 9

169
50-- LEFT SEAT

30--

'-' 10-- _X

-10--

-30--

DR]-13.65

•= .lo .15 .2o ._ .3o ._5

TIME

5O

RIGHT SEAT

30--

-I0--

-30--

DRI:13.92

-50o,,ql,,,,l,i,,l,,,,l,,,,l,,,,l,,,,l

.t.15 .I0 .15 ,_ ._ .R] .35

TIME

DYNAMIC RESPONSE INDEX

BACK TANGENT LINE

NASA TEST NO. 9

170
._o-- LEFT SEAT

30--

'_ 10--

/f---\ 1-

,-,.__.__ -. ..,.-,f-'.:___

-I[-- _ I/

/

-3o-- DR]=18.30

-50 I I I I I I I I I I I I i i I I I I I I I I I I I i i i I I I I I I I

0 .05 .I0 .IS .LX:} ._ 30 ._5

TIME

m

•_o RIGHT SEAT

30E

'-' 10--

_" f"x F

",\.,v" I ,,.,_.,,i

- j/ ,._i

-_o- DR]:16.33

-50 l I i I I I I I i [ I I I I I I I I I I I I I I I I I i I I I I I I I

.05 .I0 45 ._ -_ .90 .35

TIME

DYNAMICRESPONSE INDEX

DUMMY PELVIS Z-AXIS

NASA TEST NO. 9

171
11.0 NASATESTNO. 10

HORIZONTALVELOCITY: 0 ft/sec

VERTICALVELOCITY: 25 ft/sec

CREWMODULEPITCH: 2o

CREWFiODULEROLL: 0°

CREWMODULEYAW: 0°

LEFT SEAT: F-Ill Operationa]

RIGHTSEAT: Energy Absorbing

172
5--

z -5-

O

I--

LIJ

.-I

LU

0

0

S B

0 1"_ I I I ..J /_-- .=_C]_

z -5 _---

-10 _--

-t5 -

o .ou .o8 .12 .t_ .2o .2_

TIME (SEC)

LEFT BULKHEAD

NASA TEST NO. 10

173
TIME (SEC)

RIGHT BULKHEAD

NASA TEST NO. 10

174
5-

. .... l .... /x_.A k A r,, ^1_ _ __1.__.__ ,-_,._J_^^ ^^ A^I

Y 0 ".__v ..... v v _-v- -%., V"----w_-_ - _-_v_ v-_

Z

O

iii

/

LU

o

O

15

10

z 5

0

-5

o .o_ .08 .12 .16 .2o .2_

TIME (8EC)

LEFT SEAT PAN

NASA TEST NO. 10

175
5-

-5

lllllllll]lllllllll]lllllllll]lllllllll]lllllllll]Jllllllll]

0 .04 .08 .12 .16 .20 .24

TIME (SEC)

RIGHT SEAT PAN

NASA TEST NO. 10

176
S __

Y 0- I __..-..._1 _ .._ I.--_ _ I ___J

z

@

IIJJ

-I

LIJ

5-

0 I I , ._L..-_ fl

-

z-S_

-10 _---

-1S -

0 .0_ .08 .12 .16 ,20 .2_

TIME (SEC)

CAPSULE C.G.

NASA TEST NO. 10

177
SEAT PAN ALONG BACK TANGENT LINE

NASA TEST NO. 10

178
i

15-

m

tO m

X $--

m

0- I I I I I h.._.3_

m

5-

i

Z

o -5-

I--

I11

.J

w

< --

-5 ----

Z --

-10 _--

-15 _---

-20 -

0 .0_ .08 .12 .16 .20 .2q

TIME (SEC)

LEFT DUMMY PELVIS

NASA TEST NO. 10

179
lOX

--5 m

5-

z -S- O

W

W

o

O S h

-5

z_lO

-15

-20-

0 .04 .08 .12 .16 .20 .2_

TIME (SEC)

RIGHT DUMMY PELVIS

NASA TEST NO. 10

180
m

5-

-5-

z

o

Ire

IU

LU

o

0 5--

O_ i "-',,

-5 _---"

z _-

-10 _--

-1S _--

-20 -

'l'l'''llll',,,,,,,ii,l,,,ll,lll,,,,,,,il,,llIII,i,,,,l,,lli

0 .Ot_ .08 •12 •16 .20 ,2_

TIME (SEC)

LEFT DUMMY CHEST

NASA TEST NO. 10

181
5-

5-

z

0

<

W

--I

W

0

0 S-

<

_ o

-5 _---

Z -

-10 _---

-1S _---

-20 -

,,,,,,,,,l,,,,,,,,,l,,,,,,,,,l,,,,,,,,,I,,,,l,,l,l,,,,,,.j,,I

0 .0_ .08 .12 .16 .20 .24

TIME (SEC)

RIGHT DUMMY CHEST

NASA TEST NO. 10

182
10-

5

X O_

5

-10 -

-- _ "" - .... ",,Fl,_r_"'- ' .... _' i i i

Z

o -5-

W

W

0

o 5

0

s

z

-1S

-1S

-20 _

0 .0_ .08 .12 ,16 .20 .2_

TIME (SEC)

LEFT DUMMY HEAD

NASA TEST NO. 10

183
m

B

_ m

_ -5-

V _

z

0

i

W

W

0

0

< S-----

0

5

Z

-I0

-IS

-20 -

iillllillllltiillllllllllilillllltiillllllililJlllllllll

0 .0_ .08 .12 .16 .20 .24

TIME (SEC)

RIGHT DUMMY HEAD

NASA TEST NO. 10

184
LEFT THIGH

CENTER

,J,CO--

1200

tOO0 --

m

" 800

o 600 _--

14.

400 --

2OO

O- I I I 1

RIGHT THIGH

200 -

0 _-------- I . I I l _ I I

-200 -

0 .0_ .08 .12 .16 .20 .2_

TIME (SEC)

LEFT SEAT PAN LOADS

NASA TEST NO. 10

185
CENTER

1200 --

1000 --

m 800 --

d --

,,, _--

o 600 -- nO

u_o0--

200 --

Z_

o .____. I _ I i i _-. i

--- RIGHT THIGH

u,O0 _

200 --

O- I I _

'"i"i"l"i"i,,il,i,,,i,lil,,,,,lli,ll,j,i,,i,l,,,,lll

0 -OU_ .08 • 12 • 16 .20 .2u_

TIME (SEC)

RIGHT SEAT PAN LOADS

NASA TEST NO. 10

186
TIME (SEC)

RIGHT SEAT STROKE

NASA TEST NO. 10

187
LEFT FRONT

200 -

o- I I I I I I

-200 -

GO

,,, 200 -- LEFT CENTER

n-

:_

o_ 0 I I ( I I I

I.U --

¢r --

_. -200 -

TIME (SEC)

EXIT PORT PRESSURES

NASA TEST NO. 10

188
RIGHT FRONT 200 -

0- i I I i q

-200 -

RIGHT CENTER

200 -

__

0 i I I i I ] 13. --

W --

" -200 -

03

O3

UJ

nO.

RIGHT REAR

200 -

O- I I I I I I

-200 -

0 .0_ .08 .12 .16 .20 .2_

TIME (SEC)

EXIT PORT PRESSURES

NASA TEST NO. 10

189
5o LEFT SEAT

30--

'-' 10 /

-10--

-30--

DR]=15,2_

-50 t I I I I I I I I I I I I I I I i i I I I I I I I I I I I i I I I I I

0 .[_ .to .IS .20 ._ ._ ._5

T]MF

m

so RIGHT SEAT

30m

/-\

\\

-10--

-3o- ORI=15.62

-so,,,,I,,,,I,,,,I,,,,I,,,,I,,,,I,,,,I

TIME

DYNAMIC RESPONSE INDEX

SEAT PAN Z-AXIS

NASA TEST NO. 10

190
m

so LEFT SEAT

30--

¢"

-10--

-30--

DR]:1u_.73

,,,,I,,,,I,,,,I,,,,I,,,,I,,,,I,,,,I

0 .05 .10 .IS ._ ._ .30 .35

TIME

m

5O

RIGHT SEAT

30--

-10--

-30--

DR]:15.36

DYNAMIC RESPONSE INDEX

BACK TANGENT LINE

NASA TEST NO. 10

191
50

LEFT SEAT

30--

H lO--

f-

-lo /

-9o-- DRI=18.93

.05 .10 .IS .20 ._5 .30 .35

TIME

50

RIGHT SEAT

30--

'-"10--

n-

\\j I

-_o- \ x,,%_._.//

-3o-- DRI:17._

DYNAMIC RESPONSE INDEX

DUMMY PELVIS Z-AXIS

NASA TEST NO. 10

192
12.0 NASATEST NO. 11

HORIZONTALVELOCITY: 0 ft/sec

VERTICALVELOCITY: 25 ft/sec

CREWMODULEPITCH: 2o

CREWFIODULEROLL: 0°

CREWMODULEYAW: 0°

LEFT SEAT: F-Ill Operational

RIGHTSEAT: Energy Absorbing

193
5-

Y 0 - I I _ ,._. z'-_l 1---_---_I

_ -

z -5-

0

I--

<

w

-J

w

0

o

5-

0 I_--. I I I I ,,_

z -s_- \__

-10 _----

-15 -

,III,,,IIIIIIIIIIIIII,,,IIIIIIII,III,,II,,,IIII,,IIIIIIII,,I

0 .OUT .08 .t2 .t6 .20 .21⁄2

TIME (SEC)

LEFT BULKHEAD

NASA TEST NO. 11

194
5--

Z

0

<

J

W 5- 0

0

< 0 _ I I I I I

_

z-S_---

Z

-10--

-15 -

IIIllllllllllllllllllllllllllllllllllllllllllllllllllllllllll

0 .04 .08 .t2 .t6 .20 .24

TIME (SEC)

RIGHT BULKHEAD

NASA TEST NO. 11

195
5-

X 0 - -- ---J- ,-_,_ I ^ ^1

5-

- _ V

z -so

lrr

UJ

.-I

IJJ

o

o

15 -

10

0 I I

0 .04 .08 .12 .16 .20 .24

TIME (SEC)

LEFT SEAT PAN

NASA TEST NO. 11

196
x 0

-5

15 -

10 m

Z 5 m

o- I I I I J

0 .04 .08 .12 .16 .20 .2_

TIME (SEC)

RIGHT SEAT PAN

NASA TEST NO. 11

197
TIME (SEC)

CAPSULE CoG.

NASA TEST NO. 11

198
15 - LEFT SEAT

o- I I I

Z

0

w

w

O 15 _'- RIGHT SEAT

<

5--

O- I I I

0 .0_ .08 .12 .t6 .20 .2_

TIME (SEC)

SEAT PAN ALONG BACK TANGENT LINE

NASA TEST NO. 11

199
10-

5--

X -

J

Sin

z y 0 : _ I _v_.__l I

0

< -S--

n."

iii

..,I

LU

0

(b

,<

LEFT DUMMY PELVIS

NASA TEST NO. 11

2OO
1S10--

X SO- -.. I

Illlllllllllllllllllllllllllllllllllllll IIIII111111111111111

0 .04 .OB .t2 .16 .20 .24

TIME (SEC)

RIGHT DUMMY PELVIS

NASA TEST NO. 11

201
u

5-

- I_ I _ I

y O_^v_

B

15 mm

z

0m

I,-

r,- 5-

,--I m

o"' 0 i _ I I I I J

o

,_

-5 --

Z -

-tO _--

-t5 --

-20 -

TIME (SEC)

LEFT DUMMY CHEST

NASA TEST NO. 11

202
RIGHT DUMMY CHEST

NASA TEST NO. 11

203
S B

D

m

_- -__l,., I I 1 ...... L

x

-5

-I0 -

TIME (SEC)

LEFT DUMMY HEAD

NASA TEST NO. 11

204
5-

y 0 _ ....._,... ,y_--.-,J...................... IM. ',_4__,-^,]_ ,. _ __'_'_'__ ...... I

z

0

<

W

W

o o

o

5

z

-10

-1S

-20 --

o .o_ .08 .12 .16 .2o .24

TIME (SEO)

RIGHT DUMMY HEAD

NASA TEST NO. 11

205
LEFT THIGH

_00 -

I

-

2O0 --

o- i . j --'-Tr'_-_.±

RIGHT THIGH

200 -

-200 -

lillltilllllllllllllllllttiillllllillllliillllllillllltiilfl

0 .0Lt .08 .12 .16 .20 .2u,

TIME (SEC)

LEFT SEAT PAN LOADS

NASA TEST NO. 1 1

206
LEFT THIGH

u,00_

-

2O0--

-200 -

CENTER

I_00

1200--

1000

8OO

-2OO

RIGHT THIGH

_00-

200__

o- I _ L

-200 --

o .o_ .o8 .12 .16 .2o .2_

TIME (SEe)

RIGHT SEAT PAN LOADS

NASA TEST NO. 1 1

2O7
RIGHT SEAT STROKE

NASA TEST NO. 11

2O8
LEFT FRONT

200 -

O- I I I I I I

-200 -

LEFT CENTER

200 -

m

0 I I I I I I

W --

_ -20S -

w

LEFT REAR

200 -

O- I I I I I I

-200 -

IIIIIIIIIl]llllllllllllllllllllllllllllllllllllllllllllllllll

0 .0u_ .08 .t2 .1.6 .20 .2uL

TIME (SEC)

EXIT PORT PRESSURE

NASA TEST NO.11

209
RIGHT FRONT

200 -

0- I I I I I i

-200 -

m

a.. 200- RIGHT CENTER

ILl

n- 0 I I I I I 1

w -200 -

nO.

200 F RIGHT REAR

-200o_ I I I I I I

Jllllllllllllllllllllllllllllllllllllllllllllllllllllllllllll

0 .0u, .08 .12 .16 .20 .2u

TIME (8EC)

EXIT PORT PRESSURES

NASA TEST NO. 11

210
to-- LEFT SEAT

30--

-10m

-30--

DR]-1u_,22

-t0 I I I I I I i I I I I I I i I i I i i I I i i I I I I I I I I i I i I

•05 .I0 .15 ._ 25 ._0. .35

T]ME

so RIGHT SEAT

30--

4o- [_RI-1_.66

-50 I I I I I I I I I I I I i I I I I I I I I I I I I I I I I I I I I I I

0 .05 .10 .15 .20 .23 .30 .35

TIME

DYNAMIC RESPONSE INDEX

SEAT PAN Z-AXIS

NASA TEST NO. 1 1

211
50--

LEFT SEAT

30--

'-' I0-- :_t

-I0--

-30q

DRI:13.99

"50 I I I I I I I I I I I I I I I I I I I I I I I I I I I i i I t i i i I

•05 .I0 .15 .20 .25 .30 .35

TIME

m

5O

RIGHT SEAT

30--

-30 I

DRI=lq.qO

-SOIIIIIIIIIIIIIIIII_IIIIIIIIIIIII jiiI

0 .05 .10 .B ._ .25 ._O .35

TIME

DYNAMIC RESPONSE INDEX

BACK TANGENT LINE

NASA TEST NO. 11

212
5O

LEFT SEAT

30--

'-_ 10m

-I0-- \_ " /

z

-30-- DR1-18.05

m

5O

RIGHT SEAT

30--

10--

-_oii,llllllI,,llllll,ll,llllll_t,,,,I

0 .0_ .10 .IS .20 ._ ._0 .35

T]ME

DYNAMIC RESPONSE INDEX

DUMMY PELVIS Z-AXIS

NASA TEST NO. 11

213
13.0 NASATEST NO. 12

HORIZONTALVELOCITY: 0 ft/sec

VERTICALVELOCITY: 32 ft/sec

CREWMODULEPITCH: 2o

CREWNODULEROLL: 0°

CREWF_DULEYAW: 0°

LEFT SEAT: F-Ill Operational

RIGHTSEAT: Energy Absorbing

214
LEFT BULKHEAD

NASA TEST NO. 12

215
B

5-

- I,-_ _._.v_l Y O_ I _ Lv_._/

z

o_ 10---

UJ _

_J _

U.I --

< _

z -5 _----

-10 _---

-15 _--

-20 -

,lilllllilill,l,llllillilll,lllllilililliilliilllilllll'lill

0 .OU_ .08 .I:P .16 .20 .PL

TIME (SEC)

RIGHT BULKHEAD

NASA TEST NO. 12

216
m

x O- .... L__

Z

--S --

z I0

o I I

-5

IIIlllllllllllllllllllllllllllllllilllll IIIIIIIIIIIIIIIIIIII

0 .04 .08 .12 .16 .20 .24-

TIME (8EC)

LEFT SEAT PAN

NASA TEST NO. 12

217
10-

5

X

TIME {SEC}

RIGHT SEAT PAN

NASA TEST NO. 12

218
i

10-

5--

X 0

-10 -

CAPSULE C.G.

NASA TEST NO.12

219
SEAT PAN ALONG BACK TANGENT LINE

NASA TEST NO. 12

220
5-

y 0 I _ I I _ _J J

z

o

l0c

111

I -*'-, I I I I,,,--..-_--_ _ .-4

o _-

S _

-tO --

Z

-!5 _--

-20 --

-25 _

0 .OU= .08 .t2 .t6 .20 .21⁄2

TIME (SEC)

LEFT DUMMY PELVIS

NASA TEST NO. 12

221
x

$

0 I J

RIGHT DUMMY PELVIS

NASA TEST NO. 12

222
LEFT DUMMY CHEST

NASA TEST NO. 12

223
TIME (SEC)

RIGHT DUMMY CHEST

NASA TEST NO. 12

224
× -5

i

-tO -I

y ...I........ I I .... .... ._4__.I----. 0 _- '_=""_-............... _'_ u./_'"

Z

£ 5_--

I--

<

LIJ

LIJ

0

o -S _---

-10 _-

Z

-15 _---

I

-20 _--

I

-25 _--

I

-30 -

0 ,0u, ,08 ,1.2 ,16 ,20 ,2 u,

TIME (SEO)

LEFT DUMMY HEAD

NASA TEST NO. 12

225
X -5

-10

Y 0 E _-_-::_----I ........... -J'""*_,,-._'-'-..-!,-_.._ I ......

z

@

<

LO

.J

o 5

-5

Z

-10

-20

0 .0_ .08 .12 .16 .20 .24

TIME (SEC)

RIGHT DUMMY HEAD

NASA TEST NO. 12

226
LEFT THIGH

2O0O

1800

1600

w

0

1400 0

1200

1000

800

600

200

0 I I I I I i

llllllllllllllllll.llllllllllllllllllllllllllllllllllllllllll

0 .0_ .08 .12 .16 .20 .2u_

TIME (SEC)

LEFT SEAT PAN LOADS

NASA TEST NO. 12

227
__ RIGHT THIGH

200 -

0 - - --_. I _..---- I _ I

W --

o -200--

0

-_00-

0 .0_ .08 .12 .18 .20 .2_

TIME (SEC)

LEFT SEAT PAN LOAD

NASA TEST NO. 12

228
LEFT THIGH

400 -

2O0--

- I I I I

CENTER

1600

lqO0

1200

1000

m

800

W

0

600 0

4OO

2OO

RIGHT SEAT PAN LOADS

NASA TEST NO. 12

229
m

3-

2_m

m

W

w Z

o 0 I

-1 --

IIIIIIIIIIIIIIIIIIIIIIIIIIIIIllllllllllllllllllllllllllllllll

0 .0_ .08 .12 .16 .20 .2_

TIME (SEO)

RIGHT SEAT STROKE

NASA TEST NO. 12

230
I

so

LEFT SEAT

30--

0

\ t/€

-tO--

DR]=2£,92

-30--

-so,,,llJlillll,,I,,,lliilil,,,,I,,ijl

•05 .10 .15 .20 .25 30 .35

TIME

i

5O

RIGHT SEAT

30--

'-' 10--

-tO--

-3o- DR]:20.93

40 liIIllIllllIIIIIIIIliIIIIIIIIlIIIIl

.05 .Io .Is ._ ._ ._ ._s

TIME

DYNAMIC RESPONSE INDEX

SEAT PAN Z-AXIS

NASA TEST NO. 12

231
m

5O

LEFT SEAT

30--

_. f"N

HIo- ,I// ",, .\

-IG--

DR]:23.9t

-30--

-bU_LLI I I I I I I I I I I I I I I I I I I I I I ] I I I I I I I I I I

•06 .10 .15 .20 .'_ 30 .35

TIME

50

RIGHT SEAT

30--

--,,_\

'-' to- J%'_ \ "_

I/ ',\

•

-I0--

-_o- DR]:20.39

•W .I0 .15 20 £:5 30 .35

TIME

DYNAMIC RESPONSE INDEX

BACK TANGENT LINE

NASA TEST NO. 12

232
50--

LEFT SEAT

30I

-50 I I I I I I I I I I I I I ! J I I I I J I I I I J I i i i J i ! i i J

0 .05 .10 .15 .20 ._ .30 .35

T]ME

5O

RIGHT SEAT

30--

'-' 10--

j I

-10 _ / /'

-30- DRI :13.81

0 .05 .10 .15 .20 .25 .30 ._5

TIME

DYNAMIC RESPONSE INDEX

DUMMY PELVIS Z-AXIS

NASA TEST NO. 12

233
14.0 NASAI IBAHRSI NO. 17

HORIZONTALVELOCITY: 34 ft/sec

VERTICALVELOCITY: 32 ft/sec

CREWMODULEPITCH: 2o

CREWMODULEROLL: 0°

CREWMODULEYAW: 0°

LEFT SEAT: F-111 Operational

RIGHTSEAT: Energy Absorbing

234
LEFT BULKHEAD

NASA TEST NO. 17

235
-(!)

-

z

o

let

a:

w

..J

W

()

()

et

5

x

-5

-loL

5

-5

Z-lO

-15

-20

-25

III I I I I I I I II I I I I I I I I II I I I I I I I I II I I I I I I I " I I I I I I I I I II II I " I I I I

o .04 .08 .12 .16 .20 .24

TIME (SEC)

RIGHT BULKHEAD

NASA TEST NO. 17

236
LEFT SEAT PAN

NASA TEST NO. 17

237
Z -tO

-2O

lililliilllilllliilllllllillilllillillilllilliillllllillll

0 .0L_ ,08 .12 .115; .20 o2Li

TIME (SEC)

RIGHT SEAT PAN

NASA TEST NO, 17

238
-15

-20

-25 --

-30 -

0 .0_ .08 .12 .16 .20 .2_

TIME (SEC)

CAPSULE C.G.

NASA TEST NO. 17

239
15-

i0_

Y O_ _

5_

-10 -

-20

-25

-3O

IlllllllllIlllllllllllllllllllllllllllllIllllllllllllllllllj_

0 .04 .08 .12 .16 .20 .24

TIME (SEC)

CAPSULE C.G..

NASA TEST NO. 17

240
SEAT PAN ALONG BACK TANGENT LINE

NASA TEST NO. 17

241
5

Y

0

Z

0m 5-

<

W 0 [ _-"_

W

0

o -5--

<

E

z-lO _

Z

-15 --

Z

-20_

Z

-25--

-30-

llllllllllllllllillllllllllllllllllllllllllillllllllllil

0 .0_ ,08 .12 ,t6 .20 .2_

TIME (SEC)

LEFT DUMMY PELVIS

NASA TEST NO. 17

242
15

10

x 5

0 I I '

RIGHT DUMMY PELVIS

NASA TEST NO. 17

243
LEFT DUMMY CHEST

NASA TEST NO. 17

244
D

10 -

5

0 I I I I

-5

B

z -i0

0

< -15

W

W

o -20

0

-25_

-35 -

illliltllll[liiiilllllllllillllllllillllilllllllllllllllilll

0 .0_ .08 .12 .16 .20 .2_

TIME (SEC)

LEFT DUMMY CHEST

NASA TEST NO. 17

245
x 0 I I

-5

-5

z

-10

-15

-2O

IIIIIIIIIlllllllllllllilllllllJlllllllllllllllllillllllllllll

0 .0_ .08 .t2 .16 .20 .2Li

TIME (SEC)

RIGHT DUMMY CHEST

NASA TEST NO. 17

246
m

5-

X -5

e_ -I0

Z

0

- -15 -

<

I.u

.J

uJ

<

5-

-

__ --

0 .0_ .08 .12 .16 .20 .21⁄2

TIME (SEC)

LEFT DUMMY HEAD

NA:SA TE,ST NO. 17

247
20 -

15

I0

0 I I/ I

/

£ z -i0

W

-15

W

0

0

< -20

-25

-30

-35

-_0

ll,,ll,,,l,,,itt lll ,ll,ll,,It,llt,,l,l,,l,l,,lll,,,,l,,l,I

0 .0q .08 .12 .16 .20 .2_

TIME (SEO)

LEFT DUMMY HEAD

NASA TEST NOo 17

248
15-

10

5

x 0 _ _

Z -5

ira -i0

UJ

.J

W

o -15-

0

5

Y 0

-5

o .o_ .o8 .12 .16 .20 .2_

TIME (SEC)

RIGHT DUMMY HEAD

NASA TEST NO. 17

249
RIGHT DUMMY HEAD

NASA TEST NO. 17

250
m

5O

LEFT SEAT

30--

-50

•05 .I0 .15 .20 .25 30 ._5

TIME

5O

RIGHT SEAT

30--

'-' 10--

n_

':"<",,'C/

DR]:22.32

-30--

-50i I 11 I hLLL_ I I I I I I I I I I t I I I I I I I I i I I I t I

.(]5 .I0 .15 .2g .25 .30 35

TIME

DYNAMIC RESPONSE INDEX

SEAT PAN Z-AXIS

NASA TEST NO. 17

251
50

LEFT SEAT

\I

_,o _i.,_.i_,_i '

°-,o- _,'_I ,___ _',I_,ii

DR]:23.01

-30--

-50 11 I I I I I I I I I I I 11 I I I I I I I I I I I I I I I I I i i I

•05 .10 .15 .20 -25 30 45

T]tlE

B

eo RIGHT SEAT

30--

-!0 t /

ORI=22.08

-38--

DYNAMIC RESPONSE INDEX

BACK TANGENT LINE

NASA TEST NO. 17

252
SoLEFT SEAT

30--

'-' 10-- /_

n,'

-,o- \_,FiL/_/

-30- _¢_1_/'1/ DR]:B0.6Lt

-so""1'"11,,,,I11,,I,,,11,,,,I,1111

0 .06 .10 .15 .20 .25 30 .35

TIME

SO

RIGHT SEAT

30--

"" 10--

c_

,0

-30-- DRI=21.97

DYNAMIC RESPONSE INDEX

DUMMY PELVIS Z-AXIS

NASA TEST NO. 17

253


l. Report No. 2. Government Accession No. 3. Rectpient's Catalog No.

NASACR-3918

4. Title and Subtitle 5. Report Date

Design and Testing of an Energy-Absorbing Crewseat August 1985

for the F/FB-III Aircraft. Volume lll--Data From 6. Performing Organization Code

Crew Module Testing

8. Perfon_ing Organization Report No.

7.Author(s) TR-84428

S. Joseph Shane

10. Work Unit No. (TRAIS)

9. Performing Organization Nameand Address

Simula Inc. 11. Contract or Grant No.

10016 S. 51st Street NASI-17387

Phoenix, Arizona 85044 13. Type of Report and Period Covered

12. SponsoringAgency Name and _ddress Final Report

NationalAeronauticsand Space Administration May 1983 - May 1985

Washington,D.C. 20546

14. SponsoringAgencyCode

15. Supplementa_ Notes

Langley TechnicalMonitor: ClaudeB. Castle

NASA CR-3916 - Volume I--FinalReport

NASA CR-3917 - Volume II--DataFrom Seat Testing

16. Abstract

Over the past years, several papers and reportshave documentedthe unacceptably high injury rate during the escape sequence (includingthe ejection

and ground impact)of the crew module for F/FB-111aircraft, This report

documentsa program to determineif the injurypoLentialcould be reduced by

replacing the existingcrewseatswith energy-absorbingcrewseats. An energyabsorbingtest seat was designed usingmuch of the existingseat hardware.

An extensivedynamic seat test series,designed to dup]icatevarious crew

module ground impact conditions,was conductedat a sled test facility. Comparativetests with operationalF-111 crewseatswere also conducted. After

successfuldynamic testing of the seat, more testing was conductedwith the

seats mounted in an F-111 crew module. Both swing tests and verticaldrop

tests were conducted. The verticaldrop tests were used to obtain comparative data between the energy-absorbingand operationalseats. Volume I describes the energy-absorbingtest seat and testing conducted,and evaluates

the data from both test series. Volume II presentsthe data obtainedduring

the seat test series, while Volume Ill presentsthe data from the crew module

test series.

11. Key Words 18. DistributionStatement

Seat ImpactProtection

Crew Module RestraintSystems

Crashworthiness ImpactTests Unclassified- Unlimited

Escape Systems Subject Category05

19. SecurityClasslf.(of this report) 20. SecurityClasslf.(of this page) 21. No. of Pages 22. Price

Unclassified Unclassified 256 AI2

ForsalebytheNationaTechn l icaIlnformatSeionrvicSpr e, ingfield, Virgini2216 a !

NASA-Langley, 198

NationalAeronauticsand SPECIAL FOURTH CLASS MAIL Postageand FeesPaid

Space Administration BOOK National Aeronautics and

Space Administration

Washington, D.C. NASA-451

20546

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Penalty for Private Use, $300

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