Abstract: A wheel arm (114) for a chassis (140) of a towed howitzer system (100). The wheel arm (114) comprises a chassis coupling feature (116) centred on a wheel arm pivoting axis (160), and a wheel coupling feature (118) centred on a wheel rotation axis (162). The chassis coupling feature (116) is spaced apart from the wheel coupling feature (118). The wheel arm (114) comprises a lever engagement feature (122). The lever engagement feature (122), the wheel coupling feature (118) and the chassis coupling feature (116) are provided in series along the length of the wheel arm (114).

Abstract: A towed howitzer interchangeable between a travelling mode and a firing mode, the towed howitzer being suitable for deployment on a ground plane, the towed howitzer includes: a barrel for firing a projectile, the barrel defining a barrel axis, a cradle for holding the barrel at an azimuth and an elevation, a mechanism for varying the elevation and the azimuth of the barrel and a front leg for supporting an aiming mechanism. The front leg includes a wheel intended for contacting the ground at a foremost ground contact point; a suspension mechanism for resiliently mounting the wheel and a restraining mechanism for selectively enabling the suspension. The howitzer includes a back leg for contacting the ground at a backmost ground contact point. The back leg includes a hinging for swinging the back leg out of contact with the round.

Abstract: The invention provides a self-propelled mobile system that is characterized by a lightweight space frame chassis on which is mounted a large caliber artillery piece. The weight of the system is preferably less than 8,000 kg and the artillery piece preferably has a caliber of up to a 155 mm 52 caliber gun. The artillery piece may include a lightweight elevating and traversing mass and gun chassis mounted on a space frame vehicle, such vehicle having a weight which does not exceed 3,800 kg.