Test Equipment System Certification Performance Specifications ............................... 13
Dummy Certification without Headrest - To Be Defined ........................................... 20
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Dummy Certification without Headrest Performance Specifications ............................ 24
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No table of figures entries found.
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The BioRID Dummy Certification Procedures are to insure proper dummy performance.
These procedures include multiple tests to verify system inputs and two tests to verify dummy performance.
These include:
1.1.1
This test gives confidence the energy transfer device (ETD), test equipment system, and impact probe are going to provide consistent test inputs to the
Dummy Certification.
1.2.1
This test verifies the jacket material stiffness stays consistent through time.
1.3.1
This test verifies the material inside the pelvis has not changed over time.
1.4.1
To be defined
1.5.1
To be defined - This test insures the dummy’s neck will provide consistent test results. The test also provides evidence the damper, neck bumpers, muscle substitute springs and cable, are working correctly as a system.
1.6.1
To be defined.
A typical full dummy certification would follow these certification steps:
1) Test Equipment System Certification
2) Jacket Certification
3) Pelvis Bottom Certification
4) Head Impact Pad Certification (TBD)
5) Repeat Test Equipment System Certification
6) Dummy Certification without Headrest (TBD)
7) Dummy Certification with Headrest (TBD)
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2.1.1
Impact probe A shall be of rigid metallic construction and concentric about its longitudinal axis.
2.1.2
Impact probe A shall have a mass of 13.97 +/- 0.02 kg which includes all attached hardware. Including 1/3 of any suspension cable weight if impact probe is suspended.
2.1.3
The impacting end of the test impact probe is to be perpendicular and concentric with the longitudinal axis of the impact probe, having a flat, continuous, and non-deformable 152.4 +/- 0.25 mm diameter impact face, extending rearward a minimum of 25 mm, with an edge radius of 9.7 mm.
2.2.1
Impact probe B shall be of rigid metallic construction and concentric about its longitudinal axis.
2.2.2
Impact probe B shall have a mass of 33.55 kg +/- 0.1 kg which includes all attached hardware. Including 1/3 of any suspension cable weight if impact probe is suspended.
2.2.3
The impacting end of the impact probe, perpendicular and concentric with the longitudinal axis of the impact probe, having a flat, continuous, and nondeformable 254 +/- 0.25 mm diameter impact face with a 1mm - 2 mm thick
Polytetrafluoroethylene (PTFE) covering, extending rearward a minimum of
12.7 mm.
2.3.1
Device to transfer energy from the impact probe, section 2.1 or 2.2, to the test
equipment system, section 2.5, and shape the test equipment system
acceleration profile.
2.3.2
Mass of the ETD and ETD attachment bolts 2.90 kg +/- 0.01 kg.
2.3.3
Testing position:
2.3.3.1
ETD installed position, see Figure 1.
2.3.3.2
ETD must NOT contact any part of the test equipment system
OTHER THAN the ETD attachment fixture.
2.3.3.3
ETD side to side centerline plane parallel +/- 0.5 degrees to the line
of action plane of the impact probe, see Figure 1.
2.3.3.4
ETD line of action centerline is to be 0mm +/- 3mm horizontally and vertically with the impact probe centerline at the point of impact
when mounted to the test equipment system, see Figure 1.
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Figure 1: Test Equipment System and ETD Installed Position
2.4.1
ISO 6487:2012
2.4.2
The impact probe, section 2.1 or 2.2, acceleration is to be collected and
filtered using a Channel Class 180 phaseless filter.
2.4.3
The test equipment system, section 2.5, acceleration is to be collected and
filtered using a Channel Class 60 phaseless filter.
2.4.4
Sensors
2.4.4.1
Test equipment system……
2.4.4.2
Impact probe……
2.4.4.3
……..
2.5.1
The test equipment system is to be a rigid linear bearing guided system with a mass of 44.25 kg +/- .05 kg including all attachments that move with the system (except the ETD and ETD mounting screws)
2.5.1.1
Test equipment system installed position, see Figure 1.
2.5.2
Test equipment system to allow Jacket, Pelvis Bottom and Head Impact Pad
Certification in the ETD mounting location.
2.5.2.1
Jacket certification testing position, see Figure 2.
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Figure 2: Jacket Installed Position
2.5.2.1.1
Jacket impact attachment fixture dimensions, Figure 3.
Figure 3: Jacket Attachment Dimensions
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2.5.2.1.2
Jacket must NOT contact any part of the test equipment system OTHER THAN the jacket impact attachment fixture.
2.5.2.1.3
Jacket chest surface facing the impact probe, section 2.1.
2.5.2.1.4
Jacket Pelvis Interface Abdomen Attachment surface is to be
2.5.2.1.5
Jacket Pelvis Interface Abdomen Attachment surface to be
300mm +/- 3mm above the impact probe, section 2.1,
centerline at the point of impact, see Figure 2.
2.5.2.1.6
Jacket side to side centerline plane parallel +/- 0.5 degrees
to the line of action plane of the impact probe, section 2.1,
2.5.2.1.7
Jacket side to side centerline plane to be within +/- 3mm horizontally from the line of action plane of the impact
probe, section 2.1, see Figure 2.
2.5.2.1.8
Jacket is to be mounted to the test equipment system,
section 2.5, using the Spine-Torso Interface Pin holes in the
Jacket with the pin assemblies that came with the Torso
2.5.2.1.8.1
Spine is not used during the Jacket certification.
2.5.2.1.8.2
The Spine-Torso Interface Pins at location T2 are to be present in the jacket for weight purposes but
NOT used to mount the Jacket to the test equipment
2.5.2.1.8.3
It is acceptable to mount the Jacket through the rear split opening. Maximum mount horizontal width through jacket rear split is 102mm.
2.5.2.1.9
Combined mass of the test equipment system, section 2.5,
plus the jacket impact attachment fixture is to be
55.75 +/- .08 kg.
2.5.2.1.9.1
Does not include the jacket or the spine-torso interface pins.
2.5.2.2
Pelvis Bottom certification testing position, see Figure 4.
2.5.2.2.1
The front Spine Interface Plate attachment hole, see Figure
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Figure 4: Pelvis Bottom Installed Position
2.5.2.2.2
Pelvis impact attachment fixture dimensions, see Figure 5.
Figure 5: Pelvis Bottom Attachment Dimensions
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2.5.2.2.3
Pelvis must NOT contact any part of the test equipment system OTHER THAN the Pelvis impact attachment fixture.
2.5.2.2.4
Pelvis bottom surface facing the impact probe, section 2.1.
2.5.2.2.5
Pelvis femur openings are to be facing down.
2.5.2.2.6
Pelvis is to be mounted to the test equipment system,
section 2.5, using the (3) Pelvis to Spine Interface Plate
2.5.2.2.7
Pelvis side to side centerline plane parallel +/- 0.5 degrees
to the line of action plane of the impact probe, section 2.1,
2.5.2.2.8
Pelvis Bottom side to side centerline plane to be within
+/- 3mm horizontally from the line of action plane of the
impact probe, section 2.1, see Figure 4.
2.5.2.2.9
Combined mass of the test equipment system, section 2.5,
plus the pelvis impact attachment fixture, section 2.5.2.2, is
to be 75.35 +/- .09 kg.
2.5.2.2.9.1
Does not include the weight of the lower torso assembly.
2.5.2.3
Head Impact Pad certification testing position
2.5.2.3.1
To be defined.
2.6.1
The mass of the dummy equivalent fixed weight package including attachment hardware is 25.50 kg +/- 0.02 kg
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3.1.1
3.1.2
Energy Transfer Device (ETD), Section 2.3
3.1.3
Test Equipment System, Section 2.5
3.1.4
Dummy Equivalent Fixed Weight Package, Section 2.6
3.1.5
Impact Probe, section 2.2, Acceleration Measurement Device
3.1.6
Test Equipment System, section 2.5, Acceleration Measurement Device
3.1.7
Linear Measurement Devices
3.2.1
Insures proper Test Equipment System installation and function.
3.2.2
Figure 6 illustrates the typical test equipment system, section 2.5,
certification setup.
3.2.3
Position impact probe, section 2.2, so the impact probe centerline is parallel
+/- 0.5 degrees to the line of action plane of the impact probe, see Figure 1.
3.2.4
3.2.5
Attach the ETD, section 2.3, to test equipment system, section 2.5.
3.2.5.1
ETD, section 2.3, side to side centerline plane parallel +/- 0.5 degrees
to the line of action plane of the impact probe, section 2.2, see Figure
3.2.5.2
ETD, section 2.3, line of action centerline is to be 0mm +/- 3mm
horizontally and vertically with the impact probe centerline at the point of impact when mounted to the test equipment system,
3.2.6
Attach the dummy equivalent fixed weight package, section 2.6, to the
dummy mount on the test equipment system, section 2.5.
3.2.7
Mount the impact probe, section 2.2, acceleration measurement device on the
end of impact probe opposite to the impact face with its sensitive axis in line with the longitudinal axis of the impact probe.
3.2.8
Mount the test equipment system, section 2.5, acceleration measurement
device to the test equipment system so its sensitive axis is parallel to the longitudinal centerline of the impact probe.
3.2.9
impact probe face.
3.2.10
Ensure the test equipment system, section 2.5, has at least 500 mm of
unrestricted travel.
3.2.11
Soak all hardware in a controlled environment at any temperature between
20.6°C - 22.2°C and a relative humidity between 10 and 70 percent for a period of time no less than 4 hours prior to testing.
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3.3.1
Release the impact probe, section 2.2, so that it achieves a velocity between
4.7 m/s to 4.8 m/s at the point of impact.
3.3.2
Within 2mm of the point of impact, the impact probe, section 2.2, should be
level within +/- 0.5 degrees.
3.3.3
Time zero of the test is defined as the time of contact between the impact
probe, section 2.2, and the ETD, section 2.3, device.
3.3.4
Collect the impact probe, section 2.2, velocity.
3.3.5
Collect the impact probe, section 2.2, acceleration.
3.3.6
Collect the test equipment system, section 2.5, velocity.
3.3.7
Collect the test equipment system, section2.5, acceleration.
3.3.8
Wait at least 30 minutes between successive impacts on the ETD, section 2.3.
3.4.1
When the ETD, section 2.3, is impacted, the peak impact probe, section 2.2,
force shall not be less than 8600 N and no more than 9800 N.
3.4.2
The force shall be calculated by the product of the impact probe mass and the impact probe deceleration.
3.4.3
The peak test equipment system, section 2.5, acceleration shall not be less
than 118 m/s 2 and not more than 136 m/s 2 .
3.4.4
The peak test equipment system, section 2.5, velocity shall not be less than
2.65 m/s and not more than 2.95 m/s
3.4.5
The test equipment system, section 2.5, velocity decay between 50 ms and
150 ms shall not decay more than -1.5 (m/s)/s.
3.4.6
The test equipment system, section 2.5, certification should be completed
prior to performing the Jacket, Pelvis Bottom, and Head Impact Pad
Certifications and repeated prior to Dummy Certification.
Figure 6: Typical Test Equipment System Certification Setup
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4.1.1
4.1.2
Test Equipment System, Section 2.5
4.1.3
Jacket Attachment Mount, Section 2.5.2.1
4.1.4
Impact Probe Acceleration Measurement Device
4.1.5
Test Equipment System Acceleration Measurement Device
4.1.6
Linear Measurement Device
4.1.7
Torso Jacket Assembly
4.2.1
Jacket Certification insures consistent material stiffness amongst jackets
4.2.2
illustrates the typical jacket certification setup.
4.2.3
Position impact probe, section 2.1, so the longitudinal centerline of the
impact probe is parallel +/- 0.5 degrees to the line of action plane of the
4.2.4
Position the test equipment system, section 2.5, line of travel parallel to the
longitudinal centerline of the impact probe, see Figure 2.
4.2.5
Mount the impact probe, section 2.1, acceleration measurement device on the
end of impact probe opposite to the impact face with its sensitive axis in line with the longitudinal axis of the impact probe.
4.2.6
Mount the test equipment system, section 2.5, acceleration measurement
device to the test equipment system so its sensitive axis is parallel to the longitudinal centerline of the impact probe.
4.2.7
Remove the Torso Jacket Assembly from the dummy (jacket is to be filled with water).
4.2.7.1
Jacket mass including 15 attachment pins and water is 21.87 kg +/-
0.26 kg.
4.2.8
Attach Torso Jacket Assembly to test equipment system, section 2.5.
4.2.8.1
Jacket side to side centerline plane parallel +/- 0.5 degrees to the
line of action plane of the impact probe, section 2.1, see Figure 2.
4.2.8.2
Jacket side to side centerline plane to be within +/- 3mm horizontally from the line of action plane of the impact probe,
4.2.8.3
Jacket Pelvis Interface Abdomen Attachment surface to be 300mm
+/- 3mm above the impact probe centerline at the point of impact,
4.2.8.4
The Spine-Torso Interface Pins at location T2 are to be present in the jacket for weight purposes but NOT used to mount the Jacket to the test equipment system.
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4.2.9
While the impact probe is in its neutral state, position the test equipment
system, section 2.5, so the jacket is just touching the impact probe,
4.2.10
Ensure the test equipment system, section 2.5, has at least 500 mm of
unrestricted travel.
4.2.11
Soak all hardware in a controlled environment at any temperature between
20.6°C - 22.2°C and a relative humidity between 10 and 70 percent for a period of time no less than 4 hours prior to testing.
4.3.1
Release the impact probe, section 2.1, so that it achieves a velocity between
1.50 – 1.55 m/s.
4.3.2
Within 2mm of the point of impact, the impact probe, section 2.1, should be
level within +/- 0.5 degrees.
4.3.3
Time zero of the test is defined as the time of contact between the impact
probe, section 2.1, and the anterior surface on the jacket.
4.3.4
Collect the impact probe, section 2.1, velocity.
4.3.5
Collect the impact probe, section 2.1, acceleration.
4.3.6
Collect the test equipment system, section 2.5, velocity.
4.3.7
Collect the test equipment system, section 2.5, acceleration.
4.3.8
Collect jacket compression.
4.3.9
Wait at least 30 minutes between successive impacts on the same jacket.
4.4.1
When the anterior surface of the jacket is impacted, the peak impact probe,
section 2.1, acceleration shall not be less than 1110N and not more than
1360N.
4.4.2
4.4.3
The peak test equipment system, section 2.5, acceleration shall not be less
than 15.0 m/s 2 and not more than 18.6 m/s 2 .
4.4.4
The peak test equipment system, section 2.5, velocity shall not be less than
0.375 m/s and not more than 0.411 m/s.
4.4.5
The peak jacket compression shall not be less than 18.3mm and no more than 20.3mm.
4.4.6
The jacket is to be certified annually.
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Figure 7: Typical Jacket Certification Setup
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5.1.1
5.1.2
Test Equipment System, Section 2.5
5.1.3
Lower Torso Assembly Mount, Section 2.5.2.2
5.1.4
Dummy Equivalent Fixed Weight Package, Section 2.6
5.1.5
Impact Probe Acceleration Measurement Device
5.1.6
Test Equipment System Acceleration Measurement Device
5.1.7
Linear Measurement Device
5.1.8
Lower Torso Assembly
5.2.1
The Pelvis Bottom Certification insures consistent material stiffness amongst pelvises.
5.2.2
Figure 8 illustrates the typical pelvis bottom certification setup.
5.2.3
Position impact probe, section 2.1, so the longitudinal centerline of the
impact probe is parallel +/- 0.5 degrees to the line of action plane of the impact probe.
5.2.4
Position the test equipment system, section 2.5, line of travel parallel to the
longitudinal centerline of the impact probe, section 2.1, see Figure 4.
5.2.5
Mount the impact probe, section 2.1, acceleration measurement device on the
end of impact probe opposite to the impact face with its sensitive axis in line with the longitudinal axis of the impact probe.
5.2.6
Mount the test equipment system, section 2.5, acceleration measurement
device to the test equipment system so its sensitive axis is parallel to the longitudinal centerline of the impact probe.
5.2.7
Remove the Lower Torso Assembly from the dummy.
5.2.7.1
Lower torso assembly mass including femurs is
7.995 kg +/- 0.045 kg. - TBD
5.2.8
Attach Lower Torso Assembly to test equipment system, section 2.5.
5.2.8.1
Pelvis side to side centerline plane parallel +/- 0.5 degrees to the line
of action plane of the impact probe, section 2.1, see Figure 4.
5.2.8.2
Pelvis side to side centerline plane to be within +/- 3mm horizontally from the line of action plane of the impact probe,
5.2.8.3
The front Spine Interface Plate attachment hole, see Figure 5,
centerline is to be 23 mm +/- 3mm below the impact probe, section
2.1, centerline at the point of impact, see Figure 4.
5.2.9
While the impact probe, section 2.1, is in its neutral state, position the test
equipment system, section 2.5, so the pelvis bottom is just touching the
impact probe, section 2.1, face.
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5.2.10
Ensure the test equipment system, section 2.5, has at least 500 mm of
unrestricted travel.
5.2.11
Soak all hardware in a controlled environment at any temperature between
20.6°C - 22.2°C and a relative humidity between 10 and 70 percent for a period of time no less than 4 hours prior to testing.
5.3.1
Release the impact probe, section 2.1, so that it achieves a velocity between
1.50 – 1.55 m/s.
5.3.2
Within 2mm of the point of impact, the impact probe, section 2.1, should be
level within +/- 0.5 degrees.
5.3.3
Time zero of the test is defined as the time of contact between the impact
probe, section 2.1, and the bottom surface of the lower torso assembly.
5.3.4
Collect the impact probe, section 2.1, velocity.
5.3.5
Collect the impact probe, section 2.1, acceleration.
5.3.6
Collect the test equipment system, section 2.5, velocity.
5.3.7
Collect the test equipment system, section 2.5, acceleration.
5.3.8
Collect lower torso assembly compression.
5.3.9
Wait at least 30 minutes between successive impacts on the same lower torso assembly.
5.4.1
When the lower torso assembly is impacted on the bottom, the peak impact
probe, section 2.1, force shall not be less than 3250N and not more than
4620N.
5.4.2
The force shall be calculated by the product of the impact mass and the
impact probe, section 2.1, deceleration.
5.4.3
The peak test equipment system, section 2.5, acceleration shall not be less
than 36 m/s 2 and not more than 48.9 m/s 2 .
5.4.4
The peak lower torso assembly compression shall not be less than 17.8 mm and no more than 19.5mm.
5.4.5
The lower torso assembly is to be certified annually.
Figure 8: Typical Pelvis Bottom Certification Setup
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Note: The Head Impact Pad Certification insures consistent material stiffness amongst head impact pads for the BioRID with Headrest Certification.
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7.1.1
7.1.2
Test Equipment System, Section 2.5
7.1.3
Impact Probe Acceleration Measurement Device
7.1.4
Test Equipment System Acceleration Measurement Device
7.1.5
Upper Spine (T1) Accelerometer
7.1.6
Neck Rotation Potentiometer at the Occipital Condyle, Location A
7.1.7
Neck Rotation Potentiometer at T1, Location B
7.1.8
Upper Spine Rotation Potentiometer at T1, Location C
7.1.9
Lower Spine Rotation Potentiometer at Test Equipment System, Location D
7.1.10
Upper Neck Moment MY
7.1.11
Digital Inclinometer
7.1.12
Head Leveling Tool (referencing the skull lifting hole)
7.2.1
Figure 12 illustrates the typical dummy certification setup.
7.2.2
Figure 13 illustrates the test equipment system, section 2.5, dimensions for
the Head and Upper Torso Assembly positioning.
7.2.3
document.
7.2.4
Test equipment system, section 2.5, must pass Test Equipment System
Certification prior to performing this test.
7.2.5
Jacket must have met Jacket Certification within the last year prior to performing this test.
7.2.6
Check the dummy for any damage, loose or missing screws, loose or missing bumpers, etc.
7.2.7
Install upper neck load cell if not already in dummy.
7.2.8
Attach the dummy (without lower torso and arms) to dummy mounting plate
on the test equipment system, section 2.5.
7.2.9
Remove the head (JOHN BELOW TO PROVIDE DIFFERENT WORDING)
7.2.10
Verify the lateral angle of the occipital condyle (OC) plate is less than
+/-0.5 degrees, see Figure ?. Use the test equipment system linear guide as a zero reference. Adjust dummy if necessary.
7.2.11
Reattach the head.
7.2.12
Attach location A and location B sensors to the dummy between the T1 pin
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Figure 9: Location A and B Attachment
7.2.13
Attach location C sensor to the opposite side of the T1 pin, see Figure 10.
Figure 10: Location C Attachment
7.2.14
Attach location D sensor to test equipment system, section 2.5.
7.2.15
Install an “X” axis accelerometer to the T1 load cell, see Figure 11.
Figure 11: "X" Axis Accelerometer Attachment
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7.2.16
Position impact probe, section 2.2, so the impact probe centerline is parallel
+/- 0.5 degrees to the line of action plane of the impact probe, see Figure 1 .
7.2.17
7.2.18
Mount the impact probe, section 2.2, acceleration measurement device on the
end of impact probe opposite to the impact face with its sensitive axis in line with the longitudinal axis of the impact probe.
7.2.19
Mount the test equipment system, section 2.5, acceleration measurement
device to the test equipment system so its sensitive axis is parallel to the longitudinal centerline of the impact probe.
7.2.20
Attach ETD, section 2.3, to test equipment system, section 2.5.
7.2.20.1
ETD side to side centerline plane parallel +/- 0.5 degrees to the line
of action plane of the impact probe, see Figure 1 .
7.2.20.2
ETD line of action centerline is to be 0mm +/- 3mm horizontally and vertically with the impact probe centerline at the point of impact
when mounted to the test equipment system, see Figure 1 .
7.2.21
impact probe face.
7.2.22
Level the head fore and aft to less than +/- 0.5 degrees using the Head
Leveling Tool.
7.2.23
Ensure the test equipment system, section 2.5, has at least 500 mm of
unrestricted travel.
7.2.24
Soak all hardware in a controlled environment at any temperature between
20.6°C - 22.2°C and a relative humidity between 10 and 70 percent for a period of time no less than 4 hours prior to testing.
Figure 12: Typical Dummy Certification Setup
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Figure 13: Dummy Test Equipment System Dimensions
7.3.1
Release the impact probe, section 2.2, so that it achieves a velocity between
4.7 m/s to 4.8 m/s
7.3.2
Within 2mm of the point of impact, the impact probe, section 2.2, should be
level within +/- 0.5 degrees.
7.3.3
Time zero of the test is defined as the time of contact between the impact
probe, section 2.2, and the ETD, section2.3, device.
7.3.4
Collect the impact probe, section 2.2, acceleration.
7.3.5
Collect the test equipment system, section 2.5, acceleration.
7.3.6
Collect the T1 acceleration.
7.3.7
Collect locations A, B, C and D values.
7.3.8
Collect the upper neck moment My values.
7.3.9
Wait at least 30 minutes between successive impacts on the same dummy.
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7.4.1
When the ETD, section 2.3, is impacted, the peak impact probe, section 2.2,
force shall not be less than 8000 N and no more than 9700 N.
7.4.2
The force shall be calculated by the product of the impact probe mass and the
impact probe, section 2.2, deceleration.
7.4.3
The peak test equipment system, section 2.5, acceleration shall not be less
than 137 m/s 2 and not more than 170 m/s 2 .
7.4.4
The first peak test equipment system, section 2.5, velocity shall not be less
than 2.25 m/s and no more than 2.50 m/s between 20 ms and 30 ms.
7.4.5
The test equipment system, section 2.5, velocity shall be no less than 2.1 m/s
at 135 ms to 2.0 m/s at 140 ms and no more than 2.5 m/s at 135 ms to 2.4 m/s at 140 ms.
7.4.6
The peak T1 X Axis acceleration shall not be less than 183 m/s 2 and not more than 267 m/s 2 occurring between 18.5 ms and 30.50 ms.
7.4.7
The peak head rotation about OC (Location A) shall not be less than 11.5 degrees and not more than 16.50 degrees occurring between 25 ms and 70 ms.
7.4.8
The peak head rotation must also be between 2 degrees and -9 degrees between 125 ms and 135 ms.
7.4.9
The peak neck link rotation (Location B) shall not be less than 4.00 degrees and no more than 6.5 degrees between 18.5 ms and 28.5 ms.
7.4.10
The peak neck link rotation (Location B) must also be no less than -30.0 degrees between 98 ms and 108 ms, no less than -29.0 degrees between 165 ms and 175 ms and at no time should the data be more than -36.0 degrees.
7.4.11
The T1 rotation (Location C) must be no less than -16.5 degrees between 73 ms and 78 ms and at no time be more than -19.0 degrees.
7.4.12
The total head rotation shall not be less than -25.0 degrees between 100 ms and 110 ms and between 170 ms and 190 ms and shall not be more than -
41.0 degrees between 100 ms and 190 ms.
7.4.13
The total head rotation is the sum of head rotation (Location A) and neck link rotation (Location B)
7.4.14
The total thoracic rotation shall not be less than -10.0 degrees between 125 ms and 135 ms and shall not be more than -21.0 degrees.
7.4.15
The total thoracic rotation is the sum of T1 rotation (Location C) and lower spine rotation (Location D).
7.4.16
The maximum upper neck moment My shall less than 17.8 Nm and more than 7.7 Nm between 20 ms and 35 ms.
7.4.17
The minimum upper neck moment My shall less than -23.5 Nm and more than -15.0 Nm between 66.0 ms and 83.0 ms.
Provided by Humanetics Innovative Solutions
Draft - January 27, 2014 24
Note: This test insures the dummy will perform correctly when the head impacts a headrest during a test pulse commonly seen in sled testing.
Provided by Humanetics Innovative Solutions
Draft - January 27, 2014 25