31 784 N.m
Maximum raw torque (at 0 degrees)
120 mm cannon, approximately 1,800 kg
Engineering Brief - Experimental Demonstrator
Full technical analysis covering angle-dependent torque, hydraulic actuator sizing, manual transmission strategy, costs, and real-world feasibility.
No operational main battle tank is designed to fire at 90 degrees. Modern MBTs (Leopard 2, M1 Abrams, T-90, etc.) are typically limited to about +20 to +42 degrees. A 90-degree concept is an experimental demonstrator, not a standard military retrofit.
31 784 N.m
Maximum raw torque (at 0 degrees)
120 mm cannon, approximately 1,800 kg
2 543 N.m
Residual torque (92% counterweight)
About 92% reduction
4 238 N
Required actuator force
approximately 432 kgf - 0.6 m lever arm
51:1
Transmission ratio
2 gear stages
Tactical advantages of vertical fire
How a cannon reaching 90 degrees of elevation creates new battlefield options.
Potential engagement of low-altitude threats (helicopters, diving aircraft, loitering munitions) where a standard tank is constrained by elevation limits.
Helicopters · Aircraft · DronesFPV threats and steep top-attack vectors can be addressed with direct fire when turret elevation is sufficient.
Modern C-UAS threatAbility to engage elevated positions (roofs, upper floors, terraces) without major repositioning to recover usable elevation.
Urban overmatchDirect engagement of high-angle targets with fewer detours and reduced operational delay.
Reduced blind angleAt very high elevation, near-vertical terminal trajectories could reach targets behind cover and fortifications.
120 mm mortar-like effectA single vehicle can combine conventional direct fire with anti-air and indirect options, reducing reliance on specialized assets.
Multi-role platformExplore the brief
Static summary of the technical sections planned in the source application.
Why tanks are typically limited to around 20-40 degrees of elevation.
Torque, forces, angles, and the horizontal critical point.
Force, pressure, and piston diameter sizing.
Crank system, gearing ratio, and elevation time.
Projectile path as a function of cannon elevation angle.
Trunnion, gears, actuator geometry, and force diagrams.
Prototype demonstrator budget and cost breakdown.
Estimated implementation window between 4 and 8 weeks.
Center of gravity, vertical recoil behavior, and stability implications.
Drive systems, electronics, sensors, and safety integration.
Scientific basis and comparative MBT data points.
Confidence levels for calculations, constraints, and feasibility interpretation.
Reference families supporting formulas, mechanics, and comparative context.
This static module map combines textbook mechanics and conceptual engineering assumptions. High confidence applies to core equations; medium confidence to conversion estimates; medium-low confidence to field-level performance projections sensitive to platform condition and operational context.
Core source families include classical mechanics and ballistics literature, public armored-platform technical data, and standards-oriented engineering references for actuation, safety, and validation practice.