Thermal Protection System Design of a Reusable Launch Vehicle Using Integral Soft Objects

Aprovitola Andrea; Iuspa Luigi; Viviani Antonio

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Thermal Protection System Design of a Reusable Launch Vehicle Using Integral Soft Objects

机译：基于整体软物体的可重复使用运载火箭的热保护系统设计

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In the present paper, a modelling procedure of the thermal protection system designed for a conceptual Reusable Launch Vehicle is presented. A special parametric model, featuring a scalar field irradiated by a set of bidimensional soft objects, is developed and used to assign an almost arbitrary distribution of insulating materials over the vehicle surface. The model fully exploits the autoblending capability of soft objects and allows a rational distribution of thermal coating materials using a limited number of parameters. Applications to different conceptual vehicle configurations of an assigned thickness map, and material layout show the flexibility of the model. The model is finally integrated in the framework of a multidisciplinary analysis to perform a trajectory-based TPS sizing, subjected to fixed thermal constraints.

机译：在本文中，提出了一种为概念性可重复使用运载火箭设计的热保护系统的建模程序。开发了一种特殊的参数模型，该模型具有一组二维软物体照射的标量场，并用于在车辆表面上分配几乎任意的绝缘材料分布。该模型充分利用了软物体的自动混合功能，并允许使用有限数量的参数合理分配热涂层材料。应用于指定厚度图的不同概念车辆配置以及材料布局的应用表明了该模型的灵活性。该模型最终被集成到多学科分析的框架中，以执行基于轨迹的TPS尺寸调整，并受到固定的热约束。

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《International journal of aerospace engineering》 |2019年第2期|6069528.1-6069528.14|共14页
作者
Aprovitola Andrea; Iuspa Luigi; Viviani Antonio;
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Univ Campania Luigi Vanvitelli, Dipartimento Ingn, Via Roma 29, I-81031 Aversa, Italy;

Univ Campania Luigi Vanvitelli, Dipartimento Ingn, Via Roma 29, I-81031 Aversa, Italy;

Univ Campania Luigi Vanvitelli, Dipartimento Ingn, Via Roma 29, I-81031 Aversa, Italy;

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1. Thermal Protection System Design of a Reusable Launch Vehicle Using Integral Soft Objects [J] . Andrea Aprovitola, Luigi Iuspa, Antonio Viviani International journal of aerospace engineering . 2019,第4期

机译：使用整体软物体可重复使用的发射车辆的热保护系统设计
2. Development of Functionally Graded Coating Material for Metallic Thermal Protection System of Reusable Launch Vehicle [J] . Hanamantray Baluragi, R. K. Gupta, P. P. Sinha Transactions of the Indian Institute of Metals . 2011,第4a5期

机译：可重复使用运载火箭金属热保护系统功能梯度涂料的研制
3. Development of Functionally Graded Coating Material for Metallic Thermal Protection System of Reusable Launch Vehicle [J] . Hanamantray Baluragi, R. K. Gupta, P. P. Sinha, Transactions of the Indian Institute of Metals . 2011,第sa4a5期

机译：可重复使用运载火箭金属热保护系统功能梯度涂料的研制
4. Trajectory and Thermal Protection System Design for Reusable Launch Vehicles [C] . M. McGuire, P. Gage, E. Galloway, AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference . 2004

机译：可重复使用运载火箭的轨迹和热保护系统设计
5. Advanced metallic thermal protection systems for reusable launch vehicles. [D] . Blosser, Max Leon. 2000

机译：适用于可重复使用运载火箭的先进金属热保护系统。
6. Design and Fabrication by Thermal Imprint Lithography and Mechanical Characterization of a Ring-Based PDMS Soft Probe for Sensing and Actuating Forces in Biological Systems [O] . Tommaso Dattoma, Antonio Qualtieri, Gianmichele Epifani, 2019

机译：通过热压印光刻技术设计和制造基于环的PDMS软探针用于生物系统中的传感和驱动力。
7. Thermal Protection System Design of a Reusable Launch Vehicle Using Integral Soft Objects [O] . Andrea Aprovitola, Luigi Iuspa, Antonio Viviani 2019

机译：使用整体软物体可重复使用的发射车辆的热保护系统设计
8. A Method of Integrating Aeroheating into Conceptual Reusable Launch Vehicle Design: Evaluation of Advanced Thermal Protection Techniques for Future Reusable Launch Vehicles [R] . Olds, John R., Cowart, Kris 2001

机译：将航空加热与概念性可重复使用运载火箭设计相结合的方法：评估未来可重复使用运载火箭的先进热保护技术

Thermal Protection System Design of a Reusable Launch Vehicle Using Integral Soft Objects

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