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- cannon launched rocket 炮射火箭
- Simulation and test methods of launch dynamics of multiple launch rocket system II. 多管火箭發射動力學模擬與試驗測試方法2。
- Cramming five miniature satellites into the nose of one launch rocket has had a collateral engineering benefit. 將五顆小型衛星塞入發射火箭頭部已取得間接的工程學優勢。
- The analysis on dynamics of multiple launch rocket system(MLRS) are the premise and key for evaluating and improving the performance of MLRS. 多管火箭動力學分析是評估和提高多管火箭性能的前提和關鍵。
- The virtual prototype of new Multiple Launch Rocket System(MLRS)combined with mechanism-liquid coupling model is created by using ADAMS software. 基於ADAMS建立了機械系統和液壓系統耦合的某多管火箭發射系統虛擬樣機。
- The influence of firing orders on vibration characteristics and dispersion of fire of Multiple Launch Rocket System (MLRS) was analyzed. 研究多管火箭射擊順序對其振動特性和密集度等系統性能的影響,為優化射擊順序提高射擊密集度提供直接的方法。
- The launch was delayed by one week after JAXA said it had discovered a problem with the gas jet thruster for its launch rocket. 這顆衛星將讓學生在亞洲國家的溝通順暢，並沒有相隔的時間，好像他們在同一個教室。
- That would mean satellite and launch rocket would have to be designed in tandem, so customers could not shop around for different launch vehicles. 那就意味著衛星和助推火箭必須同步設計，這樣消費者才不會為各種發射器多番比較。
- Tank Cannon Launched Beam Rider Projectile 坦克炮發射的波束制導炮彈
- The analysis on dynamics of multiple launch rocket system (MLRS) are the premise and key for evaluating and improving the performance of MLRS. 摘要多管火箭動力學分析是評估和提高多管火箭性能的前提和關鍵。
- They frequently launch rocket and other attacks on the settler communities that they see as being so symbolic of the Israeli presence. 後者多次向定居者社區發射火箭和其它攻擊物，因為他們視其為以色列存在的象徵。
- Cramming five of miniature satellites into the nose of one launch rocket has a collateral engineering benefit. Each is a cube, less than one meter wide and high. 把5枚微型衛星擠入火箭前端有間接的工程利益。每一個立方都不足1米高和寬。
- Antitank ammunition is faced with flinty challenge, then target sensitive projectile of LMLRS (Long range Multiple Launch Rocket System) emerge as the times require. 反坦克武器面臨嚴峻的挑戰，遠程火箭末敏彈便應運而生。
- Abstract The influence of firing order and firing interval on vibration characteristic and firing dispersion of multiple launch rocket system (MLRS) was analyzed. 摘要 研究多管火箭射擊順序和射擊時間間隔對其振動特性和密集度等系統性能的影響，為優化射擊順序提高射擊密集度提供直接的方法。
- FLIGHT RELIABILITY TEST METHOD STUDY OF CANNON LAUNCHED GUIDED PROJECTILE 炮射導彈飛行可靠性試驗法研究
- Especially, one kind method--Collaborative Optimization(CO) is discussed. By applying CO in two function problems, the performance of CO is analyzed and improved. In the end of this part, CO is applied in conceptual design of launch rocket. 重點研究協同優化方法的計算特性，通過兩個簡單的函數實例分析協同優化方法的計算特性，對其不足進行改進，並將其應用於一個包含三個學科的運載火箭設計實例，實現了學科之間并行優化，得到了改善的收斂解，從而驗證協同優化方法的可行性。
- Data of the related reliability、maintainability、supportability of the launch rocket system is collected and analyzed, and it is processed according as data demand of the simulation model. 經收集分析該武器系統相關可靠性、維修性、保障性數據，並依據模擬模型的數據要求進行數據處理。
- Our fighter planes are all armed with cannon. 我們的戰鬥機都裝備了機關炮。
- The cannon shot the town to pieces. 大炮的射擊毀了這座城市。
- To evaluate the firing accuracy of weapon system by use of a little number of ammunition is the seeking target of approval test in the course of multiple launch rocket system (MLRS) development. 用較少的彈藥科學評價武器系統射擊準確度是多管火箭武器系統定型試驗追求的目標。
