Dragonlab将为太空试验提供平台，其中包括恢复压缩的和一些未压缩的载荷以及部署小太空船。
DragonLab provides a platform for in-space experimentation, including recovery of pressurized and some unpressurized payloads, as well as deployment of small spacecraft.
采用准静态压缩试验，得到不同规格的空气垫压缩后的接触面积和压缩载荷特性，并与模型理论值比较。
The quasi-static compression was employed, through which the comparison was made between the models and experimental values of the contacting areas and static compressing curves.
本研究观察了版纳小型猪近交系椎骨、肋骨的解剖学、组织学形态，并对其腰椎进行轴向载荷压缩试验。
The morphology of anatomy and histology of vertebra and rib, and vertical compression on lumbar vertebrae in inbreed line Banna mining were studied.
本研究观察了版纳小型猪近交系椎骨、肋骨的解剖学、组织学形态，并对其腰椎进行轴向载荷压缩试验。
The morphology of anatomy and histology of vertebra and rib, and vertical compression on lumbar vertebrae in inbreed line Banna minipig were studied.
根据土的物理力学性质指标，天然湿度下载荷试验和浸水载荷试验，认为：盐渍土是具有中等压缩性和湿陷性的土。
With reference to its physico-mechanical property indexes, load tests and soaking load tests at natural temperatures indicate that the salt lick soil has medium compressibility and wet depressibility.
分别采用室内回弹试验、野外平板载荷试验和堆载试验，综合确定土体的再压缩模量；
The synthesized reload modulus was confirmed by resilience test, plate loading test, and large scale bearing test. The replacement foundation modulus was ensured by the method of equivalent-stiffness.
该文以铅作为试验材料，测定单向压缩有限变形和双向受约束两种情形下的载荷位移曲线，建立了基于欧拉描述的铅有限变形本构方程。
The keypoint to simulate the metal forming process by using finite deformation theory is to define the constitutive equations of the material.
辅助夹具有效地传递了压缩载荷和扭转载荷，并保持力和力矩中心线在试验过程中始终不变。
The compressive load and torque were transferred effectively. The Central Line of the force and torque...
采用准静态压缩试验，得到不同规格的空气垫压缩后的接触面积和压缩载荷特性，并与模型理论值比较。
Simulation on quasi-static compression has been carried out to see the influence of the structural parameters used for the honeycomb composites on their capability of absorbing energy.
采用准静态压缩试验，得到不同规格的空气垫压缩后的接触面积和压缩载荷特性，并与模型理论值比较。
Simulation on quasi-static compression has been carried out to see the influence of the structural parameters used for the honeycomb composites on their capability of absorbing energy.
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