launch weight 中文意思是什麼
launch weight
解釋
運載重量-
The results showed that the thrust - weight ratio reached 1. 04 for the launch weight 5400kg in the condition of specific impulse near 600s
結果表明:在發動機工作比沖接近600s的情況下，對于起飛質量為5400kg的飛行器而言，推重比為1 . 04左右。 -
To optimize specific impulse to 700s or 800s, the thrust - weight ratio could be improved to 1. 23 or 1. 41, it is enough to achieve the launch requirement for this vehicle
進一步將比沖優化至700s或800s ，可以將推重比提高至1 . 23或1 . 41 ，這樣就完全能夠保證發射任務的完成。 -
With the development of reusable launch vehicles, the thermal protection system has been oriented by the idea of incorporate design which involves thermal protection - structure - thrust system. at the same time, the weight proportion of thermal protection system has been reduced, but the working temperature of thermal protection system has been increased
隨著可重復使用航天器的發展，熱防護系統在向著防熱-結構-推進系統一體化設計的方向發展，與此同時，整個防熱系統在總起飛重量中所佔的重量比例也在降低，而使用溫度升高，即要求防熱結構日趨先進。 -
Based on the results of the pilot programme, the cuhk diabetes and endocrine centre, under the auspices of the hong kong foundation for research and development in diabetes, and the cuhk centre for nutritional studies of the school of public health will jointly launch a self - funded 6 - month obesity management programme combining pharmacological therapy and behaviour modification to facilitate high risk obese subjects to achieve realistic weight reduction and improvement of their risk profiles
香港中文大學糖尿及內分泌中心獲香港糖尿病研究發展基金會的資助，將與中大公共衛生學院轄下的營養研究中心合辦六個月自費的體重管理計劃（ obesitymanagementprogramme ） ，根據上述研究的結果，利用藥物治療及跟進行為的方法，幫助高危的肥胖人士減輕體重及改善其健康情況。 -
By use of some eigenvalues such as missile launch location, infrared radiation of boosting missiles plumes and missile engine off - time eigenvalue, data fusion based on weight sum of membership degree is applied to deduce the type and launching country of the missile
該演算法提出用導彈發射點，位置、導彈尾焰紅外特徵和導彈關機點特徵量作為導彈目標識別的特徵量，用模糊隸屬度加權求和方式進行信息融合，根據融合和最大融合量的閾值判決確定導彈的類型、國別。
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