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Full text of "NHTSA NCAP: Volkswagen 1979 VW Rabbit 2-Door Hatchback"

REPORT NO. 6525- V- 5 



NEW CAR ASSESSMENT AND STANDARDS 

ENFORCEMENT INDICANT TESTING 

FMVSS NOS. 212, 219 AND 301-75 



VOLKSWAGEN OF AMERICA, INC. 
1979 VW RABBIT 2-DOOR HATCHBACK 
NHTSA-308-T5-441 



CALSPAN CORPORATION 

ADVANCED TECHNOLOGY CENTER 

P. 0. BOX 400 

BUFFALO, NEW YORK 14225 





July 10, 1979 
FINAL REPORT 



Prepared For 

U.S. DEPARTMENT OF TRANSPORTATION 

NATIONAL HIGHWAY TRAFFIC SAFETY ADMINISTRATION 

Enforcement 

Office of Vehicle Safety Compliance 

2100 Second Street, S. W., Transpoint Building 

Washington, D. C. 20590 



This Final Test Report was prepared for the U. S. Department 
of Transportation, National Highway Traffic Safety Administration, 
under contract number DOT-HS-8-01938. This document is dissemin- 
ated under the sponsorship of the U. S. Department of Transportation 
in the interest of information exchange. The United States 
Government assumes no liability for its contents or use thereof. 



FINAL REPORT ACCEPTED BY; 



Contract Technical Manager 



Date of Report Acceptance 



ii 6525-V-5 



J&33VAS3CS13 7SCH^Oi.OCY CSN71R 

CORPORLRTlOffHI RQ SOX a °° 3UPFALO. NEW YORK m223 TSL£PMGnS (715)632-7500 
an ARVHM OC^pamv <**»* GALSPAN / TWype: 7^0-523-1863 / T 9tex: 9 t- 2 70 



TECHNICAL REPORT STANDARD TITLE PAGE 



1. Report No. 



2. Government Accession No. 



3. Recipient's Catalog No. 



4. Titfe and Subtitle 

NEW CAR ASSESSMENT AND STANDARDS ENFORCEMENT 
INDICANT TESTING - FMVSS NOS. 212, 219 AND 301-75 



5. Report Date 

July 10, 1979 



6. Performing Organization Code 

92325 



7. Author^ Walter E. Levari, Test Engineer 

Donald A. Alianello, Hd. Experimental Operati 
Barbara J. Kelleher, Staff Associate 



ons 



8. Performing Organization Report No. 

6525- V- 5 



9. Performing Organization Name and Address 

Calspan Advanced Technology Center 

P. 0. Box 400 

Buffalo, New York 14225 



10. Work Unit No. 



11. Contract or Grant No. 

nrvr-HS-ft-nig.-M 



13. Type of Report and Period Covered 



12. Sponsoring Agency Name and Address 

U. S. Department of Transportation 

National Highway Traffic Safety Administration 

Office of Vehicle Safety Compliance 

2100 Second Street. SW. Washington, D. C. 20590 

15. Supplementary 

Reviewed: / IaJUX J^ J f r \fYrU£> < \s> Project Manager 



14. Sponsoring Agency Code 

NAD- 30 



Approved 






Hd, Transportation Research. Department 
CaTspSn Advanced Technolo gy Center 



16.- Abstract 

A frontal barrier test of a 1979 VW Rabbit, 2-Door Hatchback, was performed at 
Calspan Corporation, Advanced Technology Center, Transportation Research 
Department facility for the New Car Assessment and Standards Enforcement Indicant 
Testing of FMVSS 212 - Windshield Mounting; FMVSS 219 - Windshield Zone Intrusion; 
FMVSS 301-75 - Fuel Standard Integrity for the Office of Vehicle Safety Compliance 
the Office of Automotive Ratings and for Research and Development. 

Impact Speed was 34.8 mph. 

Post-impact maximum vehicle crush was 22.7. 

Compartment intrusion was 9.6". 

The vehicle complied in all respects with FMVSS 212, FMVSS 219 and FMVSS 301-75. 

Driver exceeded FMVSS 208 - Injury Criteria for Head and Chest. 



17. Key Words 



18. Distribution Statement 

Copies of this report are available from : 
Technical Reference Division 
National Highway Traffic Safety Admin. 
Room 5108, Nassif Building 
400 7th Street, SW, Washington, DC 20590 



19. Security Classif. (of this report} 

Unclassified 



20. Security Classif, {of this page) 

Unclassified 



21. No. of Pages 22, Price 



Form DOT F 1700.7 <a-6S> 



11 1 



6525-V-5 



TABLE OF CONTENTS 



Page No 



Section 1 Purpose and Test Procedure 

Section 2 Summary of Test Number 5 

Section 3 Summary of Results of FMVSS Nos. 212, 219 

and 301-75 



1-1 
2-1 
3-1 



Appendix A Photographs 

Appendix B Vehicle and Dummy Response Data 

Appendix C Dummy Certification Tests 



A-l 
B-l 
C-l 



IV 



A&VAtaCSD T3CHMOLQCV CENTER 



6525-V-5 



COR P O R ATION PQ BOX *°° 3UFFALO. NEW YORK 14225 TEl£?HON£ (716)632-7500 
_ Cable: CALSPAN / Teietyp«: 710-523-1863 / Teiex: 91-270 



LIST OF FIGORES 



Figure No . 



Page No 



PRE-TEST AND POST- TEST MEASUREMENT POINTS 

OCCUPANT CLEARANCE DIMENSIONS 

CAMERA POSITIONS FOR FRONTAL/OBLIQUE IMPACTS 

VEHICLE ACCELEROMETER LOCATIONS 

WINDSHIELD ZONE INTRUSION, FMVSS 219 DATA SHEET 

PROTECTED ZONE 

SUMMARY OF FMVSS 212 DATA 



2-6 

2-8 

2-9 

2-11 

3-5 

3-6 

3-7 



APPENDIX A 
1A 

2A 

3A 

4A 

SA 

6A 

7A 

8A 

9A 

10A 

11A 



FULL FRONT, SIDE, REAR AND THREE-QUARTER EXTERIOR A- 2 
VIEW 

FULL FRONT, SIDE, REAR AND THREE-QUARTER POST-VIEW A- 3 

PRE- AND POST-VIEW OF UNDERBODY A- 4 

VIEW OF FUEL PUMP AND FUEL LINES A- 5 

PRE- AND POST-VIEW OF DRIVER AND PASSENGER POSITIONS A-6 

FULL WINDSHIELD VIEW A- 7 

POST-VIEW OF WINDSHIELD CRACK A- 7 

POST-VIEW OF CHILD POSITION A- 7 

POST-VIEW OF INTERIOR A- 7 

ENGINE BLOCK ACCELEROMETER A- 8 

VELOCITY TRAP COUNTER DISPLAY A- 8 



CO R PORATION P0 3 ° x " 00 buffalo, new yohk 1422s telephone (718)632-7500 

AM AAVIIN COM(=*NV 



CUM: G4LSPAN I Teietyp*; 710-523-1863/ Te»x: 81-270 



6525-V-5 



LIST OF FIGURES - Continued 



APPENDIX C 



Figure No . p W e No , 

C-l LUMBAR SPINE FLEXION TEST APPARATUS C-13 

C-2 ABDOMEN PRESS TEST APPARATUS C-13 

C-3 HEAD DROP TEST APPARATUS C-13 

C-4 KNEE IMPACT TEST APPARATUS C-l 4 

C-5 THORAX IMPACT TEST APPARATUS C-l 4 

C-6 NECK IMPACT TEST APPARATUS C-l 4 

C-7 PART 572 TEST DUMMY - FRONT AND SIDE VIEW C-l 5 

C-8 ELECTRONIC TEST EQUIPMENT C-16 



vi 6525-V-5 



AM ARVIfSt COMPANY 



RO. BOX 400 8UFFALO. NEW YORK 14225 TELEPHONE (716)632-7500 
Cable: CALSPAN / Teletype: 710-523-1863 / Telex: 91-270 



SECTION 1 
PURPOSE AND TEST PROCEDURE 



PURPOSE: The purpose of this test was to determine whether the subject 
vehicle (a 1979 Volkswagen Rabbit, 2-Door Hatchback) meets the 
requirements of FHVSS Nos. 212, 219 and 301-75 at a higher test 
speed and also to obtain structural and dummy information 
for Research and Development and the Office of Automotive Ratings 
of the NHTSA. This test is part of the New Car Assessment Program 
B.O.A., Task 2, sponsored by the National Highway Traffic Safety 
Administration (NHTSA) under Contract DOT-HS-8-01933, 

TEST PROCEDURE: The Calspan Corporation, Advanced Technology Center, 

" Transportation Research Department Test Procedure for the New 

Car Assessment Crash Tests submitted to, and approved by, 
the Contract Technical Manager (CTM) contains the specific 
procedures used to perform this test. 

With the exception of a higher test speed, this procedure is 
not in conflict with any portion of FMVSS Procedures issued 
by the Office of Standards Enforcement and the Amendments in 
effect as noted by the applicable contract. 



1-1 6525-V-5 

^OKSP^KjATIOH PO - BOX 4G0 BUFFALO. NEW YORK 14225 TELEPHONE (716)632-7500 

Cable: CALSPAN / Tefetype: 710-523-^853 / Telex: 91-270 

AIN ARVIM COM PANY ^^ 



SECTION 2 
SUMMARY OF TEST NUMBER 5 



Test number 5 was a frontal barrier impact of a 1979 Volkswagen 
Rabbit 2-door Hatchback traveling at 34.8 mph. Table 1 presents pertinent 
crash test information. Maximum crush of the vehicle was 22.7 inches measured 
at the vehicle center! ine (position XI in Figure 1 and Table 4). The average 
crush measured from the rear surface to right side of front bumper (position X19) 
and rear surface to left side of front bumper (position X20) is 21,9 inches. 
Vehicle pre- and post-impact photographs are found in Appendix A, 

The driver and right front passenger positions were occupied by two 
Part 572 50th percentile anthropometric test devices (ATDs) and both were re- 
strained with production 2-point passive torso belt systems. An Alderson VIP-- 
6C 6-year old size ATD was positioned as the right rear passenger and restrained 
with a lap belt. These three ATDs were instrumented in the head and chest re- 
gions with triaxial accelerometers and the 50th percentile ATDs were also equipped 
with femur load cells. Dummy injury criteria measurements are presented in 
Table ,3 and the response data traces are found in Appendix B. 

The 50th percentile ATDs used in this crash had been certified prior 
to the last crash test (308-T4-440). Currently there are no certification pro- 
cedures defined for the six-year-old size ATD. Since neither of the 50th per- 
centile ATDs failed to comply with FMVSS 208 injury criteria on the previous test, 
it was not necessary to re-certify them before the current crash test (308-T5-441 ). 
All certification data are presented in Appendix C. 

Post-test observations are discussed under General Comments. 



2-1 6525-V-5 



Table 1 



CRASH TEST SUMMARY 



TEST NO. 308-15-441 



DATE 



7-10-79 



PROJECT: NEW CAR ASSESSMENT PROGRAM 



TIME: 15:39 TEMP: 78° 



VEHICLE 

TEST WEIGHT (lbs) 

IMPACT ANGLE (deg)* 

IMPACT VELOCITY (mph)** 

MAX. CRUSH (in) 

MAX. INTRUSION (in) 



1979 Volkswagen Rabbit, 2- Door Hatchback 



25Q0. 




22.7 



9.6" 



DUMMIES 



TYPE 

LOCATION 

RESTRAINT 



HYBRID II PART 572 
LF(D 



2-PQINT PASSIVE 
TORSO BELT 

NUMBER OF DATA CHANNELS 

NUMBER OF HIGH SPEED CAMERAS 



36 



HYBRID II PART 57 2 
RF(2) 

2-POINT PASSIVE 
TORSO BELT 



8 + 1 Real Ti me 



ALDERSON VIP-6C 



RR(3) 



LAP BELT 



*With respect to tow track Center! ine 
**Speed trap measurement (+ .05% accuracy) 



2-2 



6525-V- 5 



GENERAL COMMENTS 



The Volkswagen Rabbit complied with FMVSS Nos. 212, 219 and 301-75. 
There was 100% windshield retention (FMVSS 212), no windshield intrusion 
(FMVSS 219) and no fuel leakage after impact or during rollover test (FMVSS 
301-75). 

The right front passenger experienced no head contact with the vehicle 
interior and complied with FMVSS 208 injury criteria. The driver ATD did not 
comply in both the head and chest areas as he sustained contact with the steering 
wheel as the steering column was forced upward and into the occupant compartment 
during impact. The driver ATD head contacted with the hub of the steering wheel 
and ATD chest contact deformed the lower rim of the steering wheel. Steering 
wheel deformation is evident in Figure 5A and 9A. 

The 6-year old size ATD positioned as the right rear passenger and 
restrained with a lap belt generated a HIC number of over 2000 due to an apparent 
head contact with the back of the front seat. A post- test photograph of the child 
position can be reviewed in Figure 8A. 

Some general post-impact observations: 

# Vehicle complied in all respects with FMVSS Nos, 212, 
219 and 301-75. 

# Windshield damage consisted of a few central cracks 
(Figure 7A) . 

The side and rear windows remained intact. 

# Right and left front tires were pinched by vehicle 
crush but remained inflated (Figure 2A). 



2-3 6525-V-5 



Table 2 

VEHICLE TEST WEIGHTS AS TESTED 



Left Front 710 lbs Left Rear 580 lbs 

Right Front 760 lbs Right Rear 550 lbs 

Total Front 1470 lbs Total Rear 1130 lbs 



Total Weight = 1470 + 1130 = 2600 lbs 



Wheel Base = 94.5 inches 



Cg F w = 1130 lbs . 94.5 inches = 41.07 inches 
2600 lbs 



CALCULATION FOR TEST WEIGHT 



RCLW - Rated Cargo and Luggage Weight 

UDW ■= Unloaded Delivered Weight (I960 lbs) 

VCW = Vehicle Capacity Weight (362 lbs) 

DSC = Designated Seating Capacity (4) 



RCLW = VCW - 150 (DSC) 
RCLW = 862-150(4) - 262 LBS 

TEST WEIGHT = UDW + RCLW + (NO. 50th DUMMIES X 164 LBS) + (NO. 6-YEAR DUMMIES X 48 LBS) 

TEST WEIGHT = I960 + 262 + 328 + 48 
TEST WEIGHT - 2598 LBS 



2-4 6525-V-S 



Table 3 
DUMMY INJURY CRITERIA VALUES 









MAXIMUM ACCELERATION C*G") * 




HEAD 


CHEST 




PELVIS 


X 


Y 


z 


R 


X 


Y 


z 


R 


X 


Y 


z 


R 


DUMMY (1) 


-78 


-28 


72.5 


SO 


-59 


-36 


-14 


67 


'"' 








DUMMY (2) 


-11 


23 


46 


47 


-31 


23 


- 5 


33 


'H 








DUMMY (3) 


-pc; 


-67 


85 


103 


-28 


-15 


50 


52 










DUMMY (4) 





























MAXIMUM FORCE-FEMUR LOAD (LBS) 


RIGHT FEMUR 


LEFT FEMUR 


DUMMY (1) 


630 


1170 


DUMMY 12) 


14^n 


Q^7 


DUMMY (3) 






DUMMY (4) 









MAXIMUM FORCE-SEAT BELTS LOADS (LBS> 


SHOULDER STRAP 
UPPER BELT LOAD 


LAP STRAP 
RIGHT BELT LOAD 


LAP STRAP 
LEFT BELT LOAD 


DUMMY (1) 


lfl^7 






DUMMY (2) 


1R^7 






DUMMY (3) 








DUMMY (4) 











HEAD INJURY CRITERIA** 


SEVERITY INDEX 


HIC 


t., (SEC) 


t 2 (SEC) 


AVE. ACC. (g) 
*1 TOt 2 


i 

HEAD 


CHEST 


DUMMY (1) 


1023.9 


.0762 


.0945 


79.3 


1306.7 




DUMMY (2) 


A?R ft 


.0606 


.1296 


32.9 


541.5 




DUMMY (3) 


2192.5 


.0735 


.14250 


63.2 


2695.6 




DUMMY (4) 















•DEFINED AS EXCEEDING 0.003 SEC. DURATION 
••AS DEFINED IN FMVSS NO. 208 



2-5 



6525-V-5 



FIGURE 1 



PRE-TEST ANO P OST- TEST MEASUREMENT POINTS 



REAR DATUM REFERENCE 



Length 
Engine 



N - ,^. *fT\V^<^v3 J *2^- To Ed 9 e of °oor 
>Wl4,5iirr^^rX\\N ( -^H number for 
^^xl^^X8,9\ N V\\j right side and 
v\\\\Y^1VA\\\\\\\V .A! odd number for 



number for 
left side 




To Trailing Edge 
Behind Door 
(Right/Left Side) 

To Leading Edge 
in Front of Door 
(Right/Left Side) 



Ctr. of 
Str. 
Column ■*> 



X17 
o 'A' Post 



_X16__ 

To Strg. Column 



_REAR DATUM REFERENCE 
To Bottom of AT CENTER OF REAR 

r^ ' A ' p ost BUMPER 

^> :(Ri ght/ Left s i de ) 

'--To Firewall (R~i ght/ Left Side) 
TT 6525-V-2 




O SI 



a. &- 



QJ 



< 



ir 



c\j 



cj 



CO 

■5 



o 

o 

13 
> 

o 

n3 

co 



U- tt. 



LT> 



CO 
*H 

Oh 
O 

03 
CO 

UJ 
CO 



<d 
o 

S3 
4-i 

Jh 
3 
CO 

fl 
<D 



<o 



o 
cm 
-a 



in 



x: 
co 

•H 

as 

4-i 
o 

<o 

CO 



CO 



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Q 

u 

4-| 
<D 

-3 

*|— i 

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CO 

aj 

CO 

C 

*!-t 

=3 

^4 
O 

O 



4-* 
O 

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co 



CO 



^o 



o 
o 

+J 

<D 

4-1 
O 

CD 

-O 
UJ 

CO 



CO 



CO r— 

LO O 



CO 



4-t 

o 

<D 
CO 
T3 

m 



CD 

>J 

4^ 
O 

CD 
CO 

CO 

c 



■M 

CO 
*r-i 

c£ 

4-1 

o 



en 



o 



LO 
Cvj 






CD 



4-> -m 



<NJ 



O 
CM 



O 
CO 

c 

■H 

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CO 



CO 



! *r 

i £ 



LO 3 



o 
.2 

■H 

CO 

-W 

"Si 



-D S 

H i 



2-7 



6525-V-5 





DRIVER 


PASS 


HH . 


lQ.n 


lfi i? 


HW 


23.5 


?3.n 


CD 


22.7 


?4.n 


cs ■ 


m n 


N/A 


SDL 


3.7 


3.5 


SCDR 


3.9 


ft fi 




HR 


7.n 


fi.5 


HS 


a r 


ft .1 


AO 


4.5 


4.0 


HD 


7.n 


5.2 ■ 



ALL DIMENSIONS ARE IN INCHES 




FIGURE 2 OCCUPANT CLEARANCE DIMENSIONS 



2-8 



6525-V-5 



FIGURE 3 

CAMERA POSITIONS FOR FRONTAL IMPACTS 



Note: Camera information shown in Table 5 



Windshield 

Styrofoam 
Template 



Camera 5 




w ill gag 



# 



i HIMl l T 



Camera 



V! 



Real Time 
Camera 



Camera 1 



^ — Monorail 



ur 



Concrete Test Pad 



"Level" tow road 



TOP VIEW 



2-9 



6525-V-5 



CAMERA NO. 



1 

2 
3 

4 

5 

6 

7 

8 

9 



Table 5 

HIGH SPEED CAMERA INFORMATION 

308-T5-441 
1979 VW RABBIT - FRONTAL 



LOCATION 



SOUTH WIDE 

SOUTH WINDSHIELD 

SOUTH DUMMY 
NORTH DUMMY 
NORTH WIDE 
REAR DUMMY 
BARRIER FACE 
PIT FRONT 
PIT REAR 



TYPE 



FASTEX 

FASTEX 

FASTEX 

FASTEX 

HYCAM 

HYCAM 

PHOTOSONIC 

PHOTOSONIC 

PHOTOSONIC 



LENS (mm) 



25 MM 
50 MM 
50 MM 
50 MM 
25 MM 
25 MM 
8 MM 
13 MM 
13 MM 



SPEED (fps) 



1300 
1400 

NO PULSE 
1350 
1750 

NO PULSE 
1000 
975 
525 



So^H L H^^^ 



2-10 



6525- V- 5 



c 



(DiP 



r 



37.75 






!£^.7 



c 



i 
23.0 

1-/(40 



s>6 



3- 



'cC.15 



4 













ACCHliiiOME'IJiE 
NCMEZS * 


ACCZLERCMEIEE LOCATION 


DELECTICN 


X 


Y 


Z 


(?) 


Engine x 


X 


@ 


Firewall Above Steering Column J x 




X 


(5) 


Firewall At Vehicle Ceirterline x 




X 


(V) 


Front Seat ?r Cros3heam" x 






® 


Hear Seat ''Crossbeam" 


X 




X 





CG 


X 


X 


X 



The accelerometar pack number can be correlated with the vehicle response data 
traces found in Appendix B. 



Figure 4 VEHICLE ACCELEROMETER LOCATIONS 



2-11 



6525-V-5 



SECTION 3 

SUMMARY OF RESULTS 

OF FMVSS NOS. 212, 

219 AND 301-75 



SUMMARY OF TEST CONDITIONS 

POST- IMPACT DATA 

WINDSHIELD ZONE INTRUSION, FMVSS 219 

PROTECTED ZONE 

SUMMARY OF FMVSS DATA 

FUEL SYSTEM INTEGRITY POST-IMPACT 



3-1 6525-V-5 



Table 6 
SUMMARY OF TEST CONDITIONS 



T^rcf \ 



T VEHICLE INFORMATION: 



Vehicle Manufacturer: 
Make/Model : VW RARRTT 

Body style: ?.r) 00r Hatchback 

VIN: 1793857442 



VOmWflfiFN OF AMFRTCA. INC 



1212. 



NETSA No,: 



30ft-Tfi-441 



; Model Year: 

; Build Date: May 1979 

,; Color; i t /Ri hf 



Engine Data 



cylinders; 89 cm. in. 



in-ycc displacement 



Transmission Data: 



4 speed { x) Manual/ ( ) Autonatic 
Date Vehicle Received by Laboratory: June 25, 1979 



3325 GENESEE STREET, BUFFALO, N. Y 



Dealer's Naase & Address: JIM KELLY 

[DATA FROM CERTIFICATION LABEL ON IXFT POOR R£AR FACE OH 'B' POST:) 
Vehicle Manufactured By: VOLKSWAGEN OF AMERICA, INC. 

Date of Manufacture: " Mav 1979 ; V^' 1793857442 , 

GVWR: 2822 lbs.; GAWR: Front = 1609 lbs.; Rear * 1278 lb 

MXI^DED TIRE PRESSURE" LASIX ON DOCR, FCST, GLOVE BOX, ETC. 



)ATA FROM ,! RECC 



Vehicle Load: 
Up to Capacity 



FRONT REAR 
psi 



2 7 



nsi 



Vehicle Capacity: ^^^ 

Type of Seats - 3ench 

X Bucket 



155SR13 



SIZE, 



Bj C D 



CARGO LOAD = %[8]6 
TOTAL =r^ 



Split 3ench 

mbs. 
2Jib B . 



Nusber of Occupants 

(Designated Seating 

Capacity) 



Front 
21 Rear 



Total 



jwZIGHT OF TEST VZHICLI AS RECEIVED FROM ZZXlZZ (with rrax. fluids)!] 



p.; r u t ^t^+ - 



FITTU 



3 



Left Front = 
TOTAL FRONT 'WEIGHT = 
TOTAL REAR WrZGHT = 
TOTAL DELV. WEIGHT = 



lbs. 
lbs. 



Left Hear - 



(3 3 







3 


7 0, 



1 v ft 
lbs. 



Hid [j ibs. ( 66.3 g of Total Vehicle Weight) 
* bs « ( 35 . 7 # of Total Vehicle Weight) 



m 



J d d ips. ; 






^ J w ^, — 
S. w.-u-.LrO: 



Right Front = 1 1716 10 j lba. 

Left Front « 



LULiU 



lbs. 



Right Rear = 
Left Rear = 



5>5lQl^ 



518IQ 



lbs. 



TOTAL FRONT WEIGHT = 
TOTAL REAR WEIGHT = 



]lbs. ( Rfi , 5 % of Total Vehicle Weight) 



TOTAL TEST WEIGHT = |2 (6 10 JO 



I'll 13 lO j ibs. ( 43, 5 % of Total Vehicle Weight) 
lbs. 



Weight of ballast secured in vehicle trunk area = 10 10 h 1 lbs. 
TEST CONDITIONS: 

7-10-79 



Date of Test: 

Aabient Teaptrature 



; Tice of Tes 



f TftC^- 



15:39 



aci/oni 



78 



Teem. In Occ. Cormart.: 



78 



°F at impact area. 
of.; V/Shld. Kldg. Tes] 



21 



Or 



3-2 



6525-V-5 



Table 6 - Continued _^_ 

VEHICLE ATTITUDE: (all diaensions in inches) 

Delivered Attitude: K F 25" ; L F 25"- ; 5 5 25" ; L B 25" 
Test Attitude: B F 23-1 /6 L F 23-3/ 4 B E 22 ; L B 22-1/ 8 

VEHICLE TIBS DATA : 

Secemaended Cold Tire Pressure: Front = 27 psi 

Hear - 31 psi 

Beeoaaended Tire Size: 155SR1 3 

Load Range: B 

Tires on Vehicle: 155SR13 " 

Is Spare Tire a "Space Saver": NO (yes/no) 

Is Spare Tire standard equipment: YES (yes/no) 

TEST FLUID DATA: __ 

Test Fluid Type: Bed Stoddard Sol™** *g : Spec* Grav.: 0.764 

Kinematic Viscosity: n.Qfi CENTISTOKES 

Spill Point Volume: 1 n . ^ Gallons (SFV) 

Test Volume: 9.55 Gallons (90 to 92* of SP^>- 

Fuel System Capacity (data from Owner's Manual): m c; gal. 

Details of fuel system: Fuel FillPr fan is nn rinht „*r *^» nf ,„ 



Electric Fuel Pump: J<_ Yes; No; Fuel Injection: J<_ Tes: .*Tc 

Does electric fuel pump operate with ignition switch "on" and 
the engine not operating: Yes; J( No 

VEHICLE REBO OTED AND C2USH: 

Ove rall Length of Test Vehi cle: Pre-Test = 2)53 ^/Ll^ ? inches 

Post-Test= 5i31.2Al31.fi inches 



CBOSHaB 22.1 /L 21.7 



FOR FRONTAL IMPACTS, distance from front of test vehicle to 
the barrier after impact = n Q inches 

•With entire fuel system filled from fuel tank through carburetor 



3„ 3 6525-V-5 



Table 7 



PCS? IMPACT DATA - GTDS. 219 & JC1 
DATA SHUT 



PI CF TZST: EQ Frontal (90°) lisp act 

t t Cblipue ( °) Impact on □ Left (Driver's; Side 

□ Hi gnt Side 

I [ Lateral or Side Ispact on □ Left (diver's) Side 

□ Right Side 
[ [ Hear Irrcact 

DAT! OF TEST: 7- 10- 79 ; TIMS: 15:39 - ; T5MP-: 78 ° - 

73. :THTSA MO.: 308- T5- 441 ; Till: 17938574.42 



Q H2CUIHZD VIZ. 7ZLCCITT HANGZ; 34.5 to 35.5 zr?h 

$ IMPACT 7ZLCCIT3 : (traps within 5 feet of impact event) 

Trap #1 = 34.8 3tpn; Trap ,?2 * FAILED sph 

Distance from the vehicle's front bumper to the barrier face 
entering the vehicle velocity measurement device = 5ft inrhp<; 

exiting the vehicle velocity measurement device = 1ft inrhps 

% 7ZZ. STATIC CRUSH : (far Frontal and Hear Impacts Only) 

Driver's Side = 21 . 7 in*; Passenger's Side = 22. 1 

Average = 21 .9 inches 

Crush Details: 



^ 755- STATIC CHCTSH : (for Side Impacts Only) 

Amount of Crush = inches on 

Crush Details: 



'TEE. H23Cu?rS : ( frczs rigid carrier only) 

Driver's Side s 12.4 inches; Pass, Side = 11.4 inches 



Average - 11.9 inches 

$ 5ZMA5X£ : 



3 _ 4 - ■ - 6525-V-5 



FIGURE 5 

WINDSHIELD ZONE INTRUSION, FMVSS 219 
DATA SHEET 




Zero Point (0,0) FRONT 7I5W 



With the zero coordinate for the X-Y grid located at the love: 
right corner (passenger side) of the windshield, record the 
following positions: 

^X) The area that the Protected Zcne JT template was penetrated 
more ^^ .25 inches by a vehicle component other than one 
which is noraally in contact with the windshield. 

Coordinates 



NONE 



J£ Y_ 



(3) The area beneath the Protected Zone 11 that the inner surface 
of the windshield was penetrated by a vehicle component. 

Coordinates 



NONE 



{Cj Hecord any windshield retention clips or brackets used to 
insure thai: the windshield would not disengage from the boc^ 



X Y 



3-5 



6525-V-5 



FIGURE 6 PROTECTED ZONE 



22.0 » 




3 12.75 



FHCOTT 7IZW OF WINDSHIZLD 



Pro-ride all dimensions necessary to reproduce the protected zone 

Method of adhering stTrcfoaa to the windshield: 

Construction adhesive applied to window su rface and to 

brake si rig of stvrn foam. then clamped in place until dry. 



3-6 



6525-V-5 



FIGURE 7 SUMMARY OF FMVSS 212 DATA 



Details of windshield Bounting (method of retention, type of tria, ate.) 
RUBBER MOLDING HOI nTNfi WINDSHTFl n 





VINDSEIZLD PZ2JPES3Y 




PRETEST 


POST TEST 


HIGST SHE j 


69.6 


69.6 


IZFT SIDE 


69.6 


69.6 


•"TOTAL*" 


139.2 


1 39 . 2 ; 



100% 



*^ ^«ir» 



ercantl ci th 



T he s tandard requires that POST TEST be a ainisua of , „_ 

PHET2ST total periphery aeasure aeat for veh icles not equipped -with 
occupant passive restraints and { 5C cercest j for each side of the 
windshield for vehicles which are equipped with occupant passive restra; 



AEEA OF PJETZNTICN FAHDIJZ: 



1" 



1" 




3-7 



6525-V-5 






Table 8 



"FUEL SYSTEM DfraaiTY" POST- IMPACT 

test data, fmvs-s no, 301-75 



TEST VEHICLE NHTSA NO 
V3Z. KB3./14AK3/H0DEL; 



8 



T 



H r T 



TEST DATE: 



7-10-79 



1Q79 VOIKSWAfiFW RARRTT 



xast chicle fuel tank filled to 90-91* of capacity with Stoddard Solvent 
and with electric fuel pump operating (if it vill operate without engine 
operation* Part 572 test dumsri.es located at each front designated seatin* 
position. * 



A- TEST VEHICLE IMPACT TIPS: CZ2 Frontal (35 oph) 

□ Oblique (35 rah) with 
contacting ___^ 



^H Hear Moving Barrier ( 35 srph) 
CH Lateral Moving Barrier (20 3rph) 

HTEL flpTT.T.AGE MEASDBEMZHT 

1* From iiapact until vehicle 
motion ceases -----_ 



° barrier face first 

(driver /passenger) side. 




2. For 5 minute period after 
veh* motion ceases- - • . 

3- For next 25 ainutes 



(^5) + 25 



ACTUAL 


MAX. A1LOV. 





1 oz. 





5 02- 





1 os. /I oin.. 



3. TEST VEHICLE STATIC 3QLLOVE3: 

TEST HEOSMAEOH WILL HE ADEED TO TEE FCLLCVEJG STATIC ^CLLOVES 
DATA SES2ES: 

(13 5TGU3S 1QA - Rollover data for 0° to 90° test phase. 

(2) FIGURE 1CB - Hollover data for 9C° to l8C° test phase. 

(3) FIGURE 1CC - Hollover data for 18C° to 270° test phase. 
CO FIGURE 1QD - Rollover data for 270° to 3c0° test phase. 

C. SOLVENT SPILLAGE DETAILS: 



NONE 



3-8 



6525-V-5 






Table 8 A 

FMVSS NO. 301-75 STATIC 3CLLCV3 DATA SHIZT 



VIH. NETSA ID SO. 



— 

3 





8 


T 


5 


4 


4 


l 



TXST FEA5Z. 





Fuel Filler 
C« Location 




ri/ WOTS : If side fiUY, 
rotate so filler 
cap is do vn « 

I. DLTIjIHEUTSON OF SOLVIT CCLLZ3CTICK TIME PSBIOD: 




Hollover Fixture 90° Hotatioa Tiae « QT aiaites, J4 J5 j seconds 

(Spec, HaLnge = 1 t: 3 sinutas) ' 

TWZ3 301-73 Position Hold Ti=e ^ QQ ninutes, 



seconds 



TOTAL - - 

Next Whole Minute Internal 

II - FMVSS 531-75 HSCUI22SCS: 



a [ 7 | sinutes, | 4 | 5 j seconds 
8j aiautes 



\±j i. M c rcn 


3U— 










First 5 ain. 


FROM onset of rotation 


6 th. 


sin. 


7th. eia. 


3th. Ein. 
if reed. 













(23 Maxisua Allowable Solreat Spillage 



5 ounces 



1 ounce 



1 ounce 1 ounce ( 



III. ACTUAL TIST VZHICLI SCLVZNT S?ZLLAGI 







NOTS : Eecord spillage 
for whole ainute 
internals only a-s 

determined above. 



IV. SOLVENT SPILLAGZ LCCATIGN(S): 



3-9 



6525-V-5-- 



■ JlWI i icr ii Tlj— i t 1 



Table 8B 

FHYSS TO, 301-75 STATIC B0UCVE3 DATA SHZZT 



VZ5. N1TSA ID }TO* 




I* PETESMINAnOW OF SOLVZW COLIZCTICft TIKZ PSIOD : 

Sollover Fixture 9C° dotation Tise- - = [£7 ai-aut^s, I 4 | ] {seconds 
(Spec. Saage 5 1 to ; minutes) ' ' 

FHV&S 3C1-75 Position Hold Tiae = + jjTj sinutes, | | | seconds 

TCTAL : = QQ aisutes^ | 4 M I seconds 

Neat Vhole Minute Interval = HH aiautes 

(1) Tiae Period— 



First 5 sia« F2CH onset of rotation! eta. aia.|?th. sin. 



(2) Haadsun Allowable Solvent Spillage 



Sta- aia- 
if reed. 



5 ounces 



1 ouace 1 ounce 1 ounce 



X H* ACTUAL TZST VTZICLZ SCLVZNT SPILLAGS 











NCTT: Hecord spillage 
for whole minute 
intervals oalj ajs 
determined above- 



iv. scLvr?rr spillage; lccaticn(s) 



3-10 



6525-V-5 



Table 8C 
3SVSSJJ0. 301-75 STATIC SOLLCVTS CATA SE 







V2E. NKTSA 13 HO.: 


3 





8 


T 


5 


4 


4 


1 



TEST ?EASZ; 






I- n^i^MDTATION Or S0L7EOT CCLL3CTICN TIKE FS2I0D: 



Hollover Fixture SC° Rotation Tiae * [T[ ainutes, I 4 j g [seconds 

(Spec. 2ange a 1 to 3 minutes) ^^ L 

3WTSS 301-75 Position Hold Kae » [J] alaatea," | | j seconds 



TOTAL * = [7]] aiautes, | 4 j 9 | seconds 

Hext Whole Minute Interval * 



m. mix eg 



H- ravss 301-75 ^j j jjja sarrs : 

(1) Tiae Period— 



?irst 5 ais. F5CM onset of rotation 6th* ain. 


7th* nin. 


1 3th* sin* 
| if reed* 







(2J Haxisua Allowable Solvent Spillage — 



5 ounces 



1 ounce 



1 ounce 



1 ounce 



IH* ACTUAL TIST VZ2ICLZ SOLTZflT SPILLAGZ, 











NCT5 ; Hecord spillagi 
for whole ninute 
intervals onlv as 
determined above* 



17. SOLVTST SPILLAGE LCCATION(S) 



3-n 



6525-V-5 



VZH. NKTSA HJ NC 



Table 8D 

TWSS SO. 301-75 STATIC 50LL0VZH DATA SEZZT 



.1 


n 


a. 


-j. 


, 5 


.,,4 


4 


.1 



TEST PEASZ: 






I- li^u-ttCTATICN OF SOLVENT C0LL3CTICN TIH2 FEHIOD: 



2oilover Fixture 50° Sotation Time- - = HT admit as, ["> I o (seconds 
(Spec. Hange = 1 to 3 arimites) ! ' ' 

ZKVSS 301-75 Position Sold Tiae % GQ minutes," | Q | o| seconds 



TOTAL . 

Heart Whole Minute Interval- 

H. FMVS5 301-75 ^UJ J I -lMZNTS 
(1) Tisie Period— 



= [ 7 1 minutes, | 3 | 3 [ seconds 

8| minutes 



r irst 5 ain. E3CM onset of rotation! cth. srin. 



7th. sin.) 8th. sin. 
if reed. 



(2) Msodaua Allowable Solvent 



3 0TC1CSS 



1 ounce 1 ounce 1 ounce 



HI. ACTUAL TEST VEHICLE SOLVENT SPILLAGE: 











MOTS : Secord spillas; 
for whole cinute 
intervals cnl/ as 
determined above. 



~>= 



IV, SOLVENT 



AGE LCCATTCN(S) 



3-12 



6525-V-5 



APPENDIX A 
STILL PHOTOGRAPHS 



A_i 6525-V-5 



_ 



_ 





FIGURE 1A FULL FRONT, SIDE, REAR AND THREE-QUARTER EXTERIOR VIEW 

W-2 6525-V-5 



■ 





FIGURE 2A FULL FRONT, SIDE, REAR AND THREE-QUARTER POST- VIEW 

A- 3 6525- V- 5 




- 

y 

L 

- 
_ 







FIGURE 3A PRE- AND POST- VIEW OF UNDERBODY 



A- 4 



6525- Y-5 



r 







FIGURE 4A VIEW OF FUEL PUMP AND FUEL LINES 



ft- 5 



652 5- V- 5 






- 





^ 








FIGURE 5A PRE- AND POST-VIEW OF DRIVER AND PASSENGER POSITIONS 



_ 



A-6 



6525-V-5 






r 





FIGURE 6A FULL WINDSHIELD VIEW FIGURE 7A POST-VIEW OF WINDSHIELD CRACK 





FIGURE 8A POST-VIEW OF CHILD POSITION FIGURE 9A POST-VIEW OF INTERIOR 



•— 



A- 7 



6525- V- 5 




_ 



_ 





FIGURE TO* ENGINE BLOCK ACCELEROMETER 



FIGURE HA VELOCITY TRAP COUNTER DISPLAY 



- 



A-8 



6525 




APPENDIX B 
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APPENDIX C 
DUMMY CERTIFICATION TESTS 



C-l 



This test report contains results from certification tests per- 
formed on Alderson Research Laboratories Model ATD 30034, 50th percentile 
anthropomorphic test dummies, Serial Nos. 319, 320, which were completed on 
June 29 and July 2, 1979, respectively. The results indicate that the dummies 
meet all of the performance requirements of the six standard tests as specified 
in 49 CFR Part 572, Federal Register, Vol. 42, No. 25, dated February 7, 1977. 

The tests were conducted at the Dummy Certification Test Facility 
of Calspan Corporation, Advanced Technology Center. A summary of the test 
results is presented in the following tables, Table 1C through 8C along with 
the Part 572 requirements. 



C-2 



P . 572 DUMMY CALIBRATION TEST DATA 



-L 


1 


J- 



NHTSA DUMMY I.D. NO. 



LABORATORY TECHNICIAN; . RED JULIANQ 
APPROVED BY: /ty fjr^ J^>f/WK^^K ^ 



Pre-Test 
Calibration 



Post-Test 
Calibration 



Date of Dummy Calibration - ■ 

Calibration Sequential Number for Dummy 

Temperature in Lab. (Spec, = 66 to 78°F) 

Relative Humidity in Lab. (Spec. = 10 to 70*) - 



TEST PARAMETER 



1 . HEAD DROP TEST : 

a. Peak Resultant Accel 

b. Peak Lateral Accel.' 

c. Time above 100G - - 



NECK BENDING TEST : 

a. Pendulum Speed - - 

b. Pendulum Avg. Decel . 
(over t3 - t£) - ~ 

c. Peak Resultant Head 
Acceleration - - 



d. 
e. 
f. 

g- 



Pendulum Decel. ( t 2" t l^ 

Pendulum Decel . (t 3 -t 2 ) 

Pendulum Decel. (t^-tj) 

Pendulum Direction 
Reversal Time - - - - 

Max. Head Rotation - - 

Chorda! Displacement: 

Head Rotation Angle - - 



( 



Time 



Displ 



30° 



Time 



Displ 



60< 



Maximum 

( °) 



Time 



Displ 



Time 



Displ. 



Continued 



SPECIFICATION 



210 to 260G 



<10G 



0.9 to 1.5 ms 



21.5 to 25.5 fps 



20 to 24G 



26G maximum 



<3 ms 



25 to 30 ms 



<10 ms 



>123 ms 



63 to 73° 



-2 to 2 ms 



to .5 in 



25.6 to 34.4 ms 



2.1 to 3.1 in. 



40.3 to 51 .7 ms 



4.3 to 5.3 in 



53.2 to 66.3 ms 



5.0 to 6.0 in. 



C-3 



29 June 1979 



78° 
68* 



228 



1.2 



23.60 



23 



17 



27 



113 



63,5 



16 



2.8 



45 



4. 95 



61 



5.25 



p, 572 F1UMMY CALIBRATION TESTDAIA <••. Continued: 



Dummy I.D. No 



TEST PARAMETER 



SPECIFICATION 



2. NECK BENDING TEST 



Continued 

i. Chorda! Displacement 
Head Rotation Angle 



60 



30 ( 



Time 



Displ 



Time 



Displ . 



67.0 to 83,0 ms 
4,3 to 5.3 in. 



85,4 to 104,6 ms 
■2.1 to 3.1 in.,. 



Time 



101.0 to 123.0 ms 



Disol. 



-.5 to 0.5 in. 



3. ABDOMINAL COMPRESSION 
TEST : 

(Preload = 10 pounds) 

a. Force 9 1" 

b. Force @ 1,3" 



50 to 63 lbs 



73 to 88 lbs. 



LUMBAR FLEXION TEST: 

a. Force § 20° - - 

b. Force @ 30° - - 

c. Force @ 40° - - 

d. Return Angle 



CHEST IMPACT TESTS: 
a. High Speed 

(1 ) Probe Speed - ■ 

(2) Peak Delfection 

(3) Peak Resistive 
Force - - - - - 

(4) Internal - - - 
Hysteresis 



22 to 34 lbs. 



34 to 46 lbs 



46 to 58 lbs 



12° maximum 



Low Speed 

(1 ) Probe Speed - - 

(2) Peak Deflection 

(3) Peak Resistive 



21.78-22.22 fos 



1 .7" maximum 



2250 lbs. maximum 



50 to 70% 



Force 



(4) Internal 

Hvsteresis- - - 



13-86-14.14 fps 



1.1" maximum 



1450 lbs. maximum 



Pre-Test 
Calibration 




Post-Test 
Calibration 



iO to 70% 



88 



4.9 



92 



2.35 



1QQ 



je& 



M 



m 



21 



50 



6° 



21.81 



1.45 



1916 



51 



13.88 



1.0 



1201 



3Q1 



C-4 



P. 572 DUMMY CALIBRATION TEST DATA Continued 



TEST PARAMETER 

6. KNEE IMPACT TESTS; 

a. Right Side — 

(1 ) Probe Speed - - - 

(2) Maximum Force - ■ 
(2) Time Above 1000# 

b. Left Side — 
(!) Probe Speed - - ■ 

(2) Maximum Force - 

(3) Time Above 1000# 



SPECIFICATION 



6.76 to 7.04 fps 



1850 to 2500 lbs 
1 .7 ms minimum 



6.76 to 7.04 fps 



1850 to 2500 lbs, 
1 .7 ms minimum 



Dummy I.D. No 



3 


1 


_2- 



Pre-Test 
Calibration 



Post-Test 
Calibration 



6.94 



0&5CL 



ZA. 



7.03 



2M& 



C-5 



INSTRUMENT CALIBRATION INFORMATION 



DUMMY I.D. NO. 



3 


1 


9 



CALIB. SEQ. NOS. FOR DUMMY: 



A. DUMMY INSTRUMENTS: 

1. Head Accel erometers- 



a. Triaxial unit — - - - 

b. Uniaxial units 

(1) Longitudinal (A x ) - 

(2) Lateral (A ) 

(3) Vertical (A z ) 

Chest Accel erometers— 
(Vehicle Crash Test Usage) 

a. Triaxial unit ------ 

b. Uniaxial units 

(1) Longitudinal (A x ) - 

(2) Lateral (A } 

(3) Vertical (A,) - - - 



3. Chest Potentiometer - - - 

4. Femur Load Cells— 

a. Right Side - 

b. Left Side 

B. CALIB . LAB . INSTRUMENTS : 

1. Pendulum Accel erometer - - 

2. Test Probe Accel erometer - 

3. Lumbar Flexion Test Push 
Force Gauge ------- 



MANUFACTURER 



Abdominal Compression Test 
Force Gauge 

Abdominal Compression Test 
Displacement Gauge - - - - 



ENDEVCO 



ENDEVCQ 



ENDEVCO 



CEC 



ENDEVCO 



CEC 



HUMANOID 
SPECIAL 



JL£L 



GSE 



B&H 



B&H 



iLE 



BLH 



CIC 



C-6 



SERIAL 
NUMBER 



DATE LAST" 
CALIBRATED 



i DATE OF 
! NEXT 
CALIBRATION 



r,K54 



IES2. 



CE76 



17938 



CG05 



21480 



306 



310 



17547 



16928 



73141 



72952 



567-11 



JL22. 



4s2! 



4-79 



1-79 



1-79 



1-79 



1-79 



1-79 



2-79 



1-79 



1-80 



1-80 



1-80 



1-80 



1-80 



1-80 



1-80 



1-80 



1-80 



1-80 



P. 572 DUMMY CALIBRATION TEST DATA 



NHTSA DUMMY I.D. NO.: 
LABORATORY TECHNICIAN: 
APPROVED BY: /W^uS*.^/ 



3 


2 






FRED JULIANO 




Pre-Test 
Calibration 



Date of Dummy Calibration __--- 

Calibration Sequential Number for Dummy 

Temperature in Lab. (Spec, = 66 to 78°F) 

Relative Humidity in Lab. (Spec. = 10 to 70%) 



TEST PARAMETER 



1 . HEAD DROP TEST : 

a. Peak Resultant Accel. 

b. Peak Lateral Accel/ - 

c. Time above 1 OOG - - - 



NECK BENDING TEST : 

a. Pendulum Speed - - - - 

b. Pendulum Avg. Decel . 
(over t3 - t£) - - — 

c. Peak Resultant Head 
Acceleration - - - - 

Pendulum Decel. (t 2 -t-| ) 

Pendulum Decel . (tg-tg) 

Pendulum Decel . (t^-tj) 

Pendulum Direction 
Reversal Time - - - - 

h. Max. Head Rotation - - 

i. Chorda! Displacement: 

Head Rotation Angle - - 



30 



50' 



Time 



Displ 



Time 



Displ 



Time 



Maximum 

( °) 



Disol 



Time 



Displ . 



Continued 



SPECIFICATION 



2 Ju 



Post-Test 
Calibration 



y 1979 



210 to 260G 
<10G 



0.9 to 1.5 ms 



21.5 to 25.5 fps 



20 to 24G 



26G maximum 



< 3 ms 



25 to 30 ms 



<1Q ms 



> 123 ms 



63 to 73' 



-2 to 2 ms 



5 to .5 in 



25.6 to 34.4 ms 



2.1 to 3.1 in. 



40.3 to 51 .7 ms 



4.3 to 5.3 in. 



53.2 to 66.3 ms 
5.0 to 5.0 in. 



C-7 



72 
72 



212 



I£ 



/L 



23.68 



24 



18 



1.5 



26 



.7 



117 



70 



30 



2.95 



£1 



5.05 



64 



SuZ. 



o^^nriMMY- CALIBRATION TEST DATA . . , . Continued: 



TEST PARAMETER 



NECK BENDING TEST .... 
Continued 

i. Chorda! Displacement: 

Head Rotation Angle — 



SPECIFICATION 



60' 



Time 



30* 



Displ. 



Time 



Displ . 



67.0 to 83.0 ms 



4.3 to 5.3 in. 



85.4 to 104.6 ms 
2.1 to 3.1 in. 



IF 



Time 101.0 to l^TcTmF 



Displ 



.5 to 0.5 in. 



3. ABDOMINAL COMPRESSION 
TEST: 

(Preload - 10 pounds) 

a. Force 3 V 

b. Force 9 1.3" 



50 to 63 lbs 



73 to 88 lbs. 



4. LUMBAR FLEXION TEST 

a. Force @ 20° - - 

b. Force 30° - - 
c« Force 9 40° - - 
d. Return Angle 



22 to 34 lbs. 
34 to 46 lbs. 



46 to 58 lbs 



12° maximum 



5. CHEST IMPACT TESTS: 
a. High Speed 

(1 ) Probe Speed - - 

(2) Peak Delfection 

(3) Peak Resistive 
Force - - - - - 



21.78-22.22 fos 



1.7" maximum 



Dummy I.D. No. : 



2250 lbs, maximum 



(4) Internal 
Hysteresis 



b. Low Speed 

(1 } Probe Speed - - - 

(2) Peak Deflection - 

(3) Peak Resistive 
Force - - — - - 

(4) Internal 
Hysteresis- - - - 



50 to 70% 



13-86-14.14 fos 



1 . V maximum 



1450 lbs. maximum 



50 to 70% 




Pre-Test 
Calibration 



M 3 [ | 2 t 

Post-Test 
Calibration 



83 



jUEL 



103 



2^21 



44£. 



54 



76 



26 



37 



52.5 



22.03 



1.54 



2124 



54% 



14.12 



1.07 



1227.6 



50% 



1 



C-8 



P. 572 DUMMY CALIBRATION TEST DATA Continued : 



TEST PARAMETER 



6. KNEE IMPACT TESTS ; 
a. Right Side — 

(1 ) Probe Speed 

(2) Maximum Force — 

(3) Time Above 1000# 



b. Left Side — 

(1) Probe Speed 

(2) Maximum Force — 

(3) Time Above 1000# 



Dummy I.D. No 



SPECIFICATION 



6.76 to 7.04 fps 
1850 to 2500 lbs 



1 .7 ms minimum 



6.76 to 7,04 fps 



1350 to 2500 lbs 



1 J ms minimum 



Pre-Test 
Cal ibration 



km 



Post-iest 
Calibration 



_£^& 



2200 



1.9 



-&^aa 



2375 



C-9 



INSTRUMENT CALIBRATION INFORMATION 



DUMMY I.D. NO. 



_3L 


I 


XL- 



CALIB. SEQ. NOS. FOR DUMMY: 



A. DUMMY INSTRUMENTS: 

1. Head Accel erometers- 



a. Tri axial unit - - - - - 

b. Uniaxial units 

(1) Longitudinal (A x ) - 

(2) Lateral (A ) 

(3) Vertical (A z ) 

Chest Accel erometers — 
(Vehicle Crash Test Usage) 



a. Triaxial unit - - - - - 

b. Uniaxial units 

(1) Longitudinal (A x ) - 

(2) Lateral (A ) 

(3) Vertical (A.,) 

3. Chest Potentiometer 

4. Femur Load Cells — 

a. Right Side 

b. Left Side 

B. CALIB . LAB . INSTRUMENTS : 

1. Pendulum Accel erometer - - 

2. Test Probe Accel erometer - 

3. Lumbar Flexion Test Push 



MANUFACTURER 



I I DATE OF 

SERIAL DATE LAST" I NEXT 
NUMBER ICALIBRATED I CALIBRATION 



Force Gauge ------- 

Abdominal Compression Test 
Force Gauge ------- 

Abdominal Compression Test 
Displacement Gauge - - - - 



ENDEVCO 



ENDEVCO 



ENDEVCO 



CEC 



ENDEVCO 



CEC 



HUMANOID 

SPECIAL 



GSE 



GSE 



MH. 



B&H 



BLH 



BLH 



CIC 



C-10 



CL60 



CG34 



CK11 



18118 



AA07 



22292 



1-79 • 



1-79 



1-79 



4-79 



4-79 



4-79 



311 



312 



17547 



16928 



73141 



72952 



1-79 



1-79 



2z21 



1-79 



567-11 



1-80 



1-80 



1-80 



1-80 



1-80 



1-80 



1-80 



1-80 



1-80 



lz21 



1-80 



Electronic Test Equipment 

The complement of signal conditioning recording and display equipment 
used in conjunction with dummy certification testing is shown in Figure 3. 

• Oata Acquisition - Sangamo Mod 3500 H channel 
FM Tape Transport (recording Speed: 50 in/sec), 

• Data Reduction - Brush Mark 250 5-channel recorder 
or Pace X-Y plotter. 

• Signal Conditioning - Calspan designed and fabricated 
bridge amplifiers providing gain, balance, and shunt 
calibration of all sensor inputs. 

• Computational Equipment - Calspan designed and 
fabricated analog computer consisting of operational 
amplifiers in circuit configurations providing con- 
tinuous computation of acceleration vector magnitude 
and Severity Index relationships. 

• Signal Filtering - Calspan designed and fabricated 
second order active filters {6 channels) with 
selectable frequency responses consistent with SAE 
J211b Class 60, 180, 600, and 1000 requirements. 
Filters are compensated for 32:1 real time expan- 
sion resulting from data recording at 60 in/sec and 
playback at 1-7/8 in/sec. 

t Real Time Reference - Tektronix Time Mark Generator; 
1 and 10 millisecond is synchronously recorded with 
all certification data and reproduced at playback on 
all strip chart records. 



Oil 6525-V-4 



The data acquisition, reproduction, and time reference 
equipment is maintained by Cal span's Equipment and 
Standards Laboratory (SSL), which is an MBS traceable 
calibration facility. Other special purpose equipment 
is maintained by qualified test facility personnel using 
support equipment maintained and standardized by all ESL. 



C-12 6525-V-4 









_ 



- 




FIGUkE C-T 
LUMBAR SPINE FLEXION TEST APPARATUS 




FIGURE C-2 
ABDOMEN PRESS TEST APPARATUS 





FIGURE C-3 
HEAD DROP TEST APPARATUS 



C-13 



' 



- 




- 



FIGURE C-7 




FIGURE C-7 
PART 572 TEST DUMMY 
FRONT & SIDE VIEW 

C-15 







1* 




Figure ■■_-;, ELECTRONIC TEST EQUIPMENT 



C-16