Rocket projectile with supported propellant grain

• 1. 一种带有隔离帽的火箭弹点火装置 [P] . 中国专利： CN206000642U . 2017.03.08
• 2. 一种火箭弹运输箱及全地形火箭弹运输车 [P] . 中国专利： CN214747546U . 2021-11-16
• 3. ROCKET-ASSISTED PROJECTILE OR GUN-BOOSTED ROCKET WITH SUPPORTED PROPELLANT GRAIN [P] . 美国专利： US3628457A . 1971-12-21

  机译： 带有助推剂颗粒的火箭弹或弹药火箭

• 4. ROCKET ASSISTED PROJECTILE OR GUN BOOSTED ROCKET WITH SUPPORTED PROPELLANT GRAIN [P] . CA874168A . 1971-06-29

  机译： 火箭炮弹或带有助推剂谷物的炮弹火箭

• 5. Rocket Assisted Projectile or Gun Boosted Rocket with Supported Propellant Charge [P] . 英国专利： GB1198235A . 1970-07-08

  机译： 带有辅助推进剂的火箭辅助弹丸或枪支助推火箭

• 1. INFLUENCE OF THE SOLID PROPELLANT GRAINS PROCESSING ON BURNING SATE OF DOUBLE BASE ROCKET PROPELLANTS [C] . Berko Zecevic, Jasmin Terzic, Mario Baskarad New trends in Research of Energetic Materials Seminar Conference . 2004
• 2. Study of surface cracks in a simulated solid rocket propellant grain with an internal star perforation. [D] . Wang, Lei. 1992
• 3. Examination of the liver in personnel working with liquid rocket propellant [O] . Palle Petersen, Erik Bredahl, Ove Lauritsen, 1970
• 4. Performance of composite solid rocket propellants for rocket assisted projectiles (RAP) [O] . Mohamed Nawwar, Tamer Wafy, Hossam Mustafa 2016
• 5. Feasibility Studies Relative to Using New Polymers and Plastics as Inhibitors to Replace Compositions Presently Being Used with Rocket Propellant Grains of 155mm HE RAP (Rocket Assisted Projectile). [R] . brenner,walter rugg,barry 1976

• 1. On the Transient Numerical Simulation of Solid Rocket Motor by Coupling Quasi One⁃Dimension Internal Flow with Three⁃Dimension Propellant Grain Burnback [J] . Juan Duan ,Yongliang Xiong ,Ningdong Hu . 哈尔滨工业大学学报:英文版 . 2021,第5期
• 2. A new experimental way for the monitoring of the real/equivalent inservice- time of double base rocket propellant by coupling VST and PCA [J] . Salim Chelouche ,Djalal Trache ,Ilyas Maamache . Defence Technology（防务技术） . 2021,第2期
• 3. Composite Solid Rocket Propellant Based on GAP Polyurethane Matrix with Different Binder Contents [J] . Islam K .Boshra ,Ahmed Elbeih ,GUO Lin . 火炸药学报 . 2020,第004期
• 4. Overview of Physical and Chemical, Operational Properties of Nitrous Oxide Used as a Propellant for Low-thrust Rocket Engines [J] . A.A.Boryaev . 火炸药学报 . 2019,第1期
• 5. Studies on the Internal Ballistics of Composite Solid Rocket Propellants Incorporating Nano-Structured Catalysts [J] . Mukesh R. ,Sivasubramaniyam R. ,Elangovan R. R. . 航空科学与技术（英文） . 2017,第4期
• 6. 再生式液体发射药火炮中液体发射药射流的内弹道研究 [C] . 栗保明 . 中国兵工学会弹道专业委员会弹道学术交流会 . 1994
• 7. 两类带有双源项的耦合反应扩散系统和两类带有动力边界条件的抛物方程的整体适定性 [A] . 刘玉 . 2012