###### Editorial Note on [Part 572](/current/title-49/part-572?toc=1)

#### Editorial Notes:

1. For compliance provisions relating to a vehicle's conformance with the performance requirements of Standard No. 208 ([§ 571.208](/on/2024-09-24/title-49/section-571.208)) relating to the part 572 test dummy, see the “Effective Date Note” at subpart E of this part.

2. Nomenclature changes to part 572 appear at [69 FR 18803](https://www.federalregister.gov/citation/69-FR-18803), Apr. 9, 2004.

#### § 572.153 Neck-headform assembly and test procedure.

(a) The neck and headform assembly (refer to [§§ 572.150(a)(1)(ii)](/on/2024-09-24/title-49/section-572.150#p-572.150(a)(1)(ii)) and [572.150(a)(1)(iii)](/on/2024-09-24/title-49/section-572.150#p-572.150(a)(1)(iii))) for the purposes of this test consists of parts shown in CRABI neck test assembly (drawing TE-3200-100);

(b) When the neck and headform assembly, as defined in [§ 572.153(a)](/on/2024-09-24/title-49/section-572.153#p-572.153(a)), is tested according to the test procedure in [§ 572.153(c)](/on/2024-09-24/title-49/section-572.153#p-572.153(c)), it shall have the following characteristics:

(1) *Flexion.*

(i) Plane D referenced in Figure R3 of this subpart shall rotate in the direction of pre-impact flight with respect to the pendulum's longitudinal centerline not less than 75 degrees and not more than 86 degrees. Within this specified rotation corridor, the peak positive moment about the occipital condyles shall be not less than 36 N-m (26.6 ft-lbf) and not more than 45 N-m (33.2 ft-lbf).

(ii) The positive moment about the occipital condyles shall decay for the first time to 5 N-m (3.7 ft-lbf) between 60 ms and 80 ms after time zero.

(iii) The moment about the occipital condyles shall be calculated by the following formula: Moment (N-m) = My − (0.005842m) × (Fx), where My is the moment about the y-axis, Fx is the shear force measured by the neck transducer (drawing SA572 -S23) and 0.005842m is the distance from the point at which the load cell measures the force to the occipital condyle.

(2) *Extension.*

(i) Plane D referenced in Figure R4 of this subpart shall rotate in the direction of preimpact flight with respect to the pendulum's longitudinal centerline not less than 80 degrees and not more than 92 degrees. Within the specified rotation corridor, the peak negative moment about the occipital condyles shall be not more than −12 Nm (−8.9 ft-lbf) and not less than −23 N-m (−17.0 ft-lbf) within the minimum and maximum rotation interval.

(ii) The negative moment about the occipital condyles shall decay for the first time to −5 Nm (−3.7 lbf-ft) between 76 ms and 90 ms after time zero.

(iii) The moment about the occipital condyles shall be calculated by the following formula: Moment (N-m) = My − (0.005842m) × (Fx), where My is the moment about the y-axis, Fx is the shear force measured by the neck transducer (drawing SA572 -S23) and 0.005842m is the distance from the point at which the load cell measures the force to the occipital condyle.

(c) *Test procedure.*

(1) Soak the neck assembly in a controlled environment at any temperature between 20.6 and 22.2 °C (69 and 72 °F) and at any relative humidity between 10 and 70 percent for at least four hours prior to a test. These temperature and humidity levels shall be maintained throughout the testing period specified in this section.

(2) Torque the jam nut (drawing 9001336) on the neck cable (drawing ATD-6206) to 0.2 to 0.3 Nm (2-3 in-lbf).

(3) Mount the neck-headform assembly, defined in [paragraph (b)](/on/2024-09-24/title-49/section-572.153#p-572.153(b)) of this section, on the pendulum so the midsagittal plane of the headform is vertical and coincides with the plane of motion of the pendulum as shown in Figure R3 for flexion and Figure R4 for extension tests.

(i) The moment and rotation data channels are defined to be zero when the longitudinal centerline of the neck and pendulum are parallel.

(ii) The test shall be conducted without inducing any torsion of the neck.

(4) Release the pendulum and allow it to fall freely to achieve an impact velocity of 5.2 ±0.1 m/s (17.1 ±0.3 ft/s) for flexion and 2.5 ±0.1 m/s (8.2 ±0.3 ft/s) for extension measured at the center of the pendulum accelerometer at the instant of contact with the honeycomb.

(i) Time-zero is defined as the time of initial contact between the pendulum striker plate and the honeycomb material. The pendulum data channel shall be defined to be zero at this time.

(ii) Stop the pendulum from the initial velocity with an acceleration vs. time pulse which meets the velocity change as specified in the following table. Integrate the pendulum acceleration data channel to obtain the velocity vs. time curve as indicated in Table B:

Table B—Pendulum Pulse

| Time | Flexion | | Time | Extension | |
| --- | --- | --- | --- | --- | --- |
| m/s | m/s | ft/s | ms | m/s | ft/s |
| 10 | 1.6-2.3 | 5.2-7.5 | 6 | 0.8-1.2 | 2.6-3.9 |
| 20 | 3.4-4.2 | 11.2-13.8 | 10 | 1.5-2.1 | 4.9-6.9 |
| 25 | 4.3-5.2 | 14.1-17.1 | 14 | 2.2-2.9 | 7.2-9.5 |