模拟和分析在月球-地球再进入期间机组人员的胸部负荷返回月球-地球
Jiatao Wang1, Zhiyong Peng2, Yongjie Yao2
1Key Laboratory for Biomechanics and Mechanobiology of the Ministry of Education, School of Biological Science and Medical Engineering, Beihang University, Beijing, China.
Frontiers in bioengineering and biotechnology
|April 2, 2024
概括
在太空任务期间,机组人员的安全至关重要. 这项研究发现,虽然胸部骨组织在月球再进入期间是安全的,但Chang.
科学领域:
- 太空飞船工程 太空飞船工程
- 生物力学 生物力学
- 太空飞行中的人类因素
背景情况:
- 在载人登月任务中,机组人员的安全至关重要,尤其是在从直接的月球-地球轨道重返月球的关键阶段.
- 了解机组人员胸部对加速度负荷的生物力学反应对于评估潜在的伤害至关重要.
研究的目的:
- 为了分析船员的胸部生物力学反应加速负载在重新进入.
- 评估由这些负载引起的机组人员潜在伤害.
- 为了比较与阿波罗和宜5T1 (CE-5T1) 任务相关的风险.
主要方法:
- 一个验证的人类胸部的有限元素模型被开发和实验验证.
- 该模型接受了模拟阿波罗和CE-5T1任务的重新进入负载.
- 分析了加速负荷和胸部组织/器官损伤之间的相关性.
主要成果:
- 在阿波罗和CE-5T1再入境模拟中,机组人员胸部骨组织的生物力学反应保持在安全值范围内.
- 与阿波罗任务相比,CE-5T1任务的重返载荷对内部器官的风险更高.
结论:
- 月球重新进入加速负载不会对机组人员胸部骨组织造成直接损伤的风险.
- 与阿波罗任务相比,CE-5T1任务需要进一步考虑内部器官保护的安全考虑.
- 这些发现为提高机组人员安全和确保未来太空探索提供了关键数据.
相关概念视频
Impact: Problem Solving
223
In an experiment conducted during a Mars mission, a rover propels a projectile with an initial velocity, and the projectile rebounds after colliding with the Martian surface. To ascertain the maximum height attained by the projectile after this collision, the known restitution coefficient and acceleration due to gravity are employed.
By designating the launch point as the origin and utilizing kinematic equations, the vertical component of the projectile's velocity at the point of impact is...
By designating the launch point as the origin and utilizing kinematic equations, the vertical component of the projectile's velocity at the point of impact is...
223
Stress: General Loading Conditions
308
To grasp the intricacy of real-world conditions where multiple loads are applied simultaneously to a structure, one might visualize a section passing through a specific point within a body, aligned parallel to the xy plane. This section is subjected to various forces, including original loads, normal forces, and shearing forces.
The shearing force, possessing potential directionality within the plane of the section, is simplified into two component forces running parallel to the x and y axes....
The shearing force, possessing potential directionality within the plane of the section, is simplified into two component forces running parallel to the x and y axes....
308
Rocket Propulsion in Gravitational Field - II
2.3K
A rocket's velocity in the presence of a gravitational field is decreased by the amount of force exerted by Earth's gravitational field, which opposes the motion of the rocket. If we consider thrust, that is, the force exerted on a rocket by the exhaust gases, then a rocket's thrust is greater in outer space than in the atmosphere or on a launch pad. In fact, gases are easier to expel in a vacuum.
A rocket's acceleration depends on three major factors, consistent with the...
A rocket's acceleration depends on three major factors, consistent with the...
2.3K
Residual Stresses in Bending
167
In the study of elastoplastic members subjected to bending moments, understanding the loading and unloading phases is crucial for assessing material behavior and structural integrity. During the loading phase, as the bending moment increases, the material initially responds elastically, adhering to Hooke's Law, where stress is directly proportional to strain. When the load exceeds the yield strength, plastic deformation occurs, resulting in permanent strain and deformation that remains even...
167
Free-falling Bodies: Example
15.9K
An object falling without any air resistance under the influence of gravitational force is said to be in free-fall. For free-falling bodies, the acceleration due to gravity is constant, irrespective of their mass. Free-fall is experienced not only by objects falling downward, but also by all objects whose motion is influenced by gravitational force alone. The dynamics of free-fall motion can be calculated using kinematic equations of motion, since free-fall acceleration is constant.
The...
The...
15.9K
Rocket Propulsion in Empty Space - I
3.2K
The driving force for the motion of any vehicle is friction, but in the case of rocket propulsion in space, the friction force is not present. The motion of a rocket changes its velocity (and hence its momentum) by ejecting burned fuel gases, thus causing it to accelerate in the direction opposite to the velocity of the ejected fuel. In this situation, the mass and velocity of the rocket constantly change along with the total mass of ejected gases. Due to conservation of momentum, the...
3.2K


