CAJ | 학술논문

基于再生式液体炮（ RLPG）及差动原理，提出了一种提高炮射智能弹药初速的新型随行装药方案，其特点是能在保持射弹过载不变条件下，大幅度提高火炮工作容积利用率和初速。这种装药技术便于与次口径脱壳弹设计技术匹配，设计出高升阻比滑翔弹，从而更有利于提高火炮的射程。导出了差动随行装药火炮内弹道模型。数值计算表明，160 mm口径火炮采用这种新型装药方案，在限定最大膛压为350 MPa、射弹底部最大压力为 p2 m≤318 MPa、飞行弹重为43．4 kg及弹丸行程为7．64 m 的条件下，取随行药量9．2 kg、主装药量13．41 kg，弹丸初速相对常规装药可提高26％，火炮工作容积利用率提高约28％。飞行弹丸采用次口径滑翔弹时，弹径为130 mm，采用修正质点外弹道模型计算得到的火炮最大射程可增大到99 km。
기우재생식액체포（ RLPG）급차동원리，제출료일충제고포사지능탄약초속적신형수행장약방안，기특점시능재보지사탄과재불변조건하，대폭도제고화포공작용적이용솔화초속。저충장약기술편우여차구경탈각탄설계기술필배，설계출고승조비활상탄，종이경유리우제고화포적사정。도출료차동수행장약화포내탄도모형。수치계산표명，160 mm구경화포채용저충신형장약방안，재한정최대당압위350 MPa、사탄저부최대압력위 p2 m≤318 MPa、비행탄중위43．4 kg급탄환행정위7．64 m 적조건하，취수행약량9．2 kg、주장약량13．41 kg，탄환초속상대상규장약가제고26％，화포공작용적이용솔제고약28％。비행탄환채용차구경활상탄시，탄경위130 mm，채용수정질점외탄도모형계산득도적화포최대사정가증대도99 km。
A new charge concept for increasing intelligent ammunition muzzle velocity based on differential traveling charge tech-nology which is able to largely increase gun working volume utilization rate and muzzle velocity within the limits of given projec-tile overload was proposed. With adaption of sub-caliber sabot projectile design technology,this charge technique facilitates the design of high lift-drag ratio gliding projectile,and increases artillery range. A differential traveling principle interior ballistic nu-meric model was established. Assuming traveling charge mass 9. 2 kg and main principal charge mass 13. 41 kg,the calculation of 160 mm gun with the new charge technique demonstrates that the projectile muzzle velocity increases by 26% and gun working volume utilization rate increases by 28%,and under the conditions of maximum bore pressure up to 350 MPa,projectile bottom maximum pressure p2m≤318 MPa,projectile mass 43. 4 kg and travel 7. 64 m. Through calculation with modified particle external trajectory model for 130mm sub-caliber gliding projectile,this charge technique can extend maximum range to 99 km.