Mechanical System Simulation of the XM307 Advanced Crew Served Weapon

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National Defense Industrial Association Joint Services Small Arms Systems Annual Symposium May 7-10 2007 Mechanical System Simulation of the XM307 Advanced Crew Served Weapon Presenter: Callista Rodriguez Principal Design Engineer- Mechanical Analyst General Dynamics ATP, Burlington VT Phone:(802)657-6536 email: crodrigu@gdatp.com DISTRIBUTION A- Unlimited

XM307 Lightweight portable crew served weapon Fires 25mm air-bursting or armor piercing ammunition Low recoil achieved with double acting buffer and unique operating cycle Tripod or vehicle mount 2

XM312.50 caliber variant used to speed development efforts 25mm airburst ammunition in parallel development.50 caliber ammunition impulse similar to 25mm.50 caliber ammunition provides a cost effective development tool 3

XM307 Firing from Tripod 4

Design Objective / Approach Objectives: Modern lightweight self-powered crew served weapon Minimize recoil to fire accurately from un-ballasted tripod Fire effectively between ±70 degrees attitude within operating environments Minimize development time Approach: Utilize Mechanical Simulation to evaluate design options Incorporates rapid design evaluation Provides good balance between performance objectives Allows evaluation of large number of design options 5

Mechanical Simulation Dynamic Model Non-Linear Rigid Body Model Characteristics: 48 Kinematic DOF Mass, cg and inertia of all parts Critical structural stiffness Friction and clearances System model: Evaluates performance Calculates interface loads Model includes the following system elements: Double acting buffer Main spring Bolt locking mechanism Firing mechanism Ammunition impulse Gas pressure/ unlocking mechanism Cartridge feeding Case eject forces 6

Mechanical Simulation Mounted on Tripod Stability assessed with un-ballasted tripod in gunner seated position Tripod model Mass, cg and inertia and stiffness included: tripod and feeder Front foot allowed to lift Weapon fires from consistent position shot to shot contributing to low dispersion 7

Characterization Firing Tests Performed in Fixture Barrel Extension Displacement and velocity High Speed Video and LVDT Transmitted Loads Double acting Buffer and Main Spring System Parameters Gas Pressure Ejection Loads Feeding Torque XM307 in firing fixture Performed in Tripod Stability assessed by leg lift measurement 8

Simulation Model Correlated to Development Weapon Test Data Barrel Extension Displacement Barrel Extension Velocity Firing at 70 deg attitude displacement Firing at 0 deg attitude Velocity time Buffer Force time Tripod Leg Lift FD S test data model scaled firing pulse Force leg lift time time Good Correlation Red Test Data Blue Analysis 9

Application of Simulation to Design Design Goals Operate successfully at -70 degrees attitude including impulse variation Maintain firing stability from tripod at 0 deg attitude Application of Simulation: Perform evaluation of sensitivity and inter-relationships of design and environmental parameters Identify and control key parameters Choose parameters to balance conflicting design goals Key design parameters to achieve goals involve double acting buffer Simulation increased buffer design efficiency 22 buffer designs investigated including variation of impulse in 3 week period Selected buffer design fabricated and tested in 3 weeks 10

Results: Successful Burst Firing of XM312 at -70 Degrees Attitude Performance goals achieved with selected buffer Fired 3 bursts of 6 rounds each XM312 Firing at -70 deg attitude displacement time burst 402 burst 404 burst 405 11

Summary Mechanical system simulation was successfully applied to ACSW weapon development Rapid turnaround of buffer design achieved with mechanical system simulation Design goals achieved Weapon fires successfully at -70 degrees attitude Weapon is stable with accurate fire while on tripod 12