2. Problem 2 For the Front Landing Gear Module, it is specified that a spring is required to soften the wheel forces transmitted to the aircraft. The only location for this

spring has been identified as indicated in green in Figure 4 with the following restriction and conditions: SEE DETAIL A- Static Length (L) Minimum Length (L_min) 80mm 30 mm 20 DETAIL A SCALE 1:1 Figure 4: Front Landing Gear Module Spring Position a. Design a suitable spring which is able to cater for all loading conditions.