[Code of Federal Regulations]
[Title 49, Volume 5]
[Revised as of October 1, 2002]
From the U.S. Government Printing Office via GPO Access
[CITE: 49CFR572.11]

[Page 762-769]
 
                        TITLE 49--TRANSPORTATION
 
                            OF TRANSPORTATION
 
PART 572--ANTHROPOMORPHIC TEST DEVICES--Table of Contents
 
                     Subpart B--50th Percentile Male
 
Sec. 572.11  Test conditions and instrumentation.

    (a) The test probe used for thoracic and knee impact tests is a 
cylinder 6 inches in diameter that weighs 51.5 pounds including 
instrumentation. Its impacting end has a flat right face that is rigid 
and that has an edge radius of 0.5 inches.
    (b) Accelerometers are mounted in the head on the horizontal 
transverse bulkhead shown in the drawings subreferenced under assembly 
No. SA 150 M010 in Figure 1, so that their sensitive axes intersect at a 
point in the midsagittal plane 0.5 inches above the horizontal bulkhead 
and 1.9 inches ventral of the vertical mating surface of the skull with 
the skull cover. One accelerometer is aligned with its sensitive axis 
perpendicular to the horizontal bulkhead in the midsagittal plane and 
with its seismic mass center at any distance up to 0.3 inches superior 
to the axial intersection point. Another accelerometer is aligned with 
its sensitive axis parallel to the horizontal bulkhead and perpendicular 
to the midsagittal plane, and with its seismic mass center at any 
distance up to 1.3 inches to the left of the axial intersection point 
(left side of dummy is the same as that of man). A third accelerometer 
is aligned with its sensitive axis parallel to the horizontal bulkhead 
in the midsagittal plane, and with its seismic mass center at any 
distance up to 1.3 inches dorsal to the axial intersection point.
    (c) Accelerometers are mounted in the thorax by means of a bracket 
attached to the rear vertical surface (hereafter ``attachment surface'') 
of the thoracic spine so that their sensitive axes intersect at a point 
in the midsagittal plane 0.8 inches below the upper surface of the plate 
to which the neck mounting bracket is attached and 3.2 inches 
perpendicularly forward of the surface to which the accelerometer 
bracket is attached. One accelerometer has its sensitive axis oriented 
parallel to the attachment surface in the midsagittal plane, with its 
seismic mass center at any distance up to 1.3 inches inferior to the 
intersection of the sensitive axes specified above. Another 
accelerometer has its sensitive axis oriented parallel to the attachment 
surface and perpendicular to the midsagittal plane, with its seismic 
mass center at any distance up to 0.2 inches to the right of the 
intersection of the sensitive axes specified above. A third 
accelerometer has its sensitive axis oriented perpendicular to the 
attachment surface in the midsagittal plane, with its seismic mass 
center at any distance up to 1.3 inches dorsal to the intersection of 
the sensitive axes specified above. Accelerometers are oriented with the 
dummy in the position specified in Sec. 572.11(i).
    (d) A force-sensing device is mounted axially in each femur shaft so 
that the transverse centerline of the sensing element is 4.25 inches 
from the knee's center of rotation.
    (e) The outputs of acceleration and force-sensing devices installed 
in the dummy and in the test apparatus specified by this part are 
recorded in individual data channels that conform to

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the requirements of SAE Recommended Practice J211a, December 1971, with 
channel classes as follows:

    (1) Head acceleration--Class 1000.
    (2) Pendulum acceleration--Class 60.
    (3) Thorax acceleration--Class 180.
    (4) Thorax compression--Class 180.
    (5) Femur force--Class 600.

    (f) The mountings for sensing devices have no resonance frequency 
within a range of 3 times the frequency range of the applicable channel 
class.
    (g) Limb joints are set at 1g, barely restraining the weight of the 
limb when it is extended horizontally. The force required to move a limb 
segment does not exceed 2g throughout the range of limb motion.
    (h) Performance tests are conducted at any temperature from 66 
deg.F to 78  deg.F and at any relative humidity from 10 percent to 70 
percent after exposure of the dummy to these conditions for a period of 
not less than 4 hours.
    (i) For the performance tests specified in Secs. 572.8, 572.9, and 
572.10, the dummy is positioned in accordance with Figure 11 as follows:
    (1) The dummy is placed on a flat, rigid, smooth, clean, dry, 
horizontal, steel test surface whose length and width dimensions are not 
less than 16 inches, so that the dummy's midsagittal plane is vertical 
and centered on the test surface and the rearmost points on its lower 
legs at the level of the test surface are at any distance not less than 
5 inches and not more than 6 inches forward of the forward edge of the 
test surface.
    (2) The pelvis is adjusted so that the upper surface of the lumbar-
pelvic adapter is horizontal.
    (3) The shoulder yokes are adjusted so that they are at the midpoint 
of their anterior-posterior travel with their upper surfaces horizontal.
    (4) The dummy is adjusted so that the rear surfaces of the shoulders 
and buttocks are tangent to a transverse vertical plane.
    (5) The upper legs are positioned symmetrically about the 
midsagittal plane so that the distance between the knee pivot bolt heads 
is 11.6 inches.
    (6) The lower legs are positioned in planes parallel to the 
midsagittal plane so that the lines between the midpoint of the knee 
pivots and the ankle pivots are vertical.
    (j) The dummy's dimensions, as specified in drawing number SA 150 
M002, are determined as follows:
    (1) With the dummy seated as specified in paragraph (i) of this 
section, the head is adjusted and secured so that its occiput is 1.7 
inches forward of the transverse vertical plane with the vertical mating 
surface of the skull with its cover parallel to the transverse vertical 
plane.
    (2) The thorax is adjusted and secured so that the rear surface of 
the chest accelerometer mounting cavity is inclined 3 deg. forward of 
vertical.
    (3) Chest and waist circumference and chest depth measurements are 
taken with the dummy positioned in accordance with paragraphs (j) (1) 
and (2) of this section.
    (4) The chest skin and abdominal sac are removed and all following 
measurements are made without them.
    (5) Seated height is measured from the seating surface to the 
uppermost point on the head-skin surface.
    (6) Shoulder pivot height is measured from the seating surface to 
the center of the arm elevation pivot.
    (7) H-point locations are measured from the seating surface to the 
center of the holes in the pelvis flesh covering in line with the hip 
motion ball.
    (8) Knee pivot distance from the backline is measured to the center 
of the knee pivot bolt head.
    (9) Knee pivot distance from floor is measured from the center of 
the knee pivot bolt head to the bottom of the heel when the foot is 
horizontal and pointing forward.
    (10) Shoulder width measurement is taken at arm elevation pivot 
center height with the centerlines between the elbow pivots and the 
shoulder pivots vertical.
    (11) Hip width measurement is taken at widest point of pelvic 
section.
    (k) Performance tests of the same component, segment, assembly, or 
fully assembled dummy are separated in time by a period of not less than 
30 minutes unless otherwise noted.
    (l) Surfaces of dummy components are not painted except as specified 
in this part or in drawings subtended by this part.

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[38 FR 20451, Aug. 1, 1973, as amended at 42 FR 7153, Feb. 7, 1977]