Sr. NO. | TEST | Pipe Length | FORCES/MOMNTS | STRESSES(N/m^2) | DEFLECTION(mm) | FACTOR OF SAFETY | 1. | Static test | Front-3.71mcockpit-8.22mRear-4.75 | Front -80.8625Driver cockpit-85.12Rear -105.26 | Minimum-0Maximum-98,584,128 | Minimum-10^-30Maximum-2.216 | Fos- 4.67 | 2. | Static front impact test | Front-3.71mcockpit-8.22mRear-4.75Impact area-.3048m | Front-80.8625N/mDriver cockpit-85.12N/mRear -105.26N/mFront Impact-750N | Minimum-9028.4Maximum-134,849,856 | Minimum-10^-30Maximum-2.66 | Fos-3.4 | 3. | Static rear impact test | Front-3.71mcockpit-8.22mRear-4.75Impact area-1.1m | Front-80.8625N/mcockpit-85.12N/mRear -105.26N/mRear Impact-750N | Minimum-9028.4Maximum-142,731,808 | Minimum-10^-30Maximum-2.769 | Fos-3.2 | 4. | Static side impact test | Front-3.71mcockpit-8.22mRear-4.75Impact area-1.778m | Front –80.8625N/mcockpit-85.12N/mRear-105.26N/mSide Impact-750N | Minimum-9028.4Maximum-138,228,816 | Minimum-10^-30Maximum-2.668 | Fos-3.3 | 5. | Bump test | Front-3.71mcockpit-8.22mRear-4.75 | Diagonally fixFront-202.15N/mDriver cockpit-215N/mRear-263.15N/m | Minimum-9028.4Maximum-434,007,232 | Minimum-10^-30Maximum-21.82 | Fos-1.1 | 6. | Torsion test | Front-3.71mcockpit-8.22mRear-4.75 | Rear portion fixLeft front force-255N(u)Right front fore-255N(d)Front –202.15N/mCockpit-215N/mEngine-263.15N/m | Minimum-0Maximum-809,534,464 | Minimum-10^-30Maximum-116.2 | Fos-0.57 |