Structural design, qualification and post-flight assessment of Crew Module Fairing

Singh Nishant; Sajeev R. K.; Ayyappadas P.; Beena A. P.; Krishnadasan C. K.

首页> 外文期刊>Current Science: A Fortnightly Journal of Research >Structural design, qualification and post-flight assessment of Crew Module Fairing

【24h】

Structural design, qualification and post-flight assessment of Crew Module Fairing

机译：船员模块整流罩的结构设计，资格和飞行后评估

获取原文

获取原文并翻译 | 示例

掌桥外文数据库（机构版） >>

开具论文收录证明 >>

文献代查 >>

页面导航

摘要
著录项
相似文献
相关主题

摘要

Crew Module Fairing (CMF) for Pad Abort Test (PAT) of Crew Escape System (CES) is configured and designed with the objective of flight qualifying necessary features like external aerodynamic shape, thermal protection system, along with Escape Motors (namely Low-altitude Escape Motor (LEM) and High-altitude Escape Motor (HEM)), with interfaces simulated as in actual flight. For improving the aerodynamic stability of the vehicle, four grid fins are attached at the aft end of CMF. Interfaces for mounting LEM, HEM, grid fins along with its deployment mechanisms and Crew Module through CM-CES attachment have been provided on CMF.

机译：用于乘员逃生系统（CES）Pad中止试验（PAT）的乘员模块整流罩（CMF）的配置和设计，其目的是验证必要的飞行特性，如外部空气动力学形状、热防护系统，以及逃生电机（即低空逃生电机（LEM）和高空逃生电机（HEM）），接口模拟为实际飞行。为了提高车辆的气动稳定性，在CMF的后端安装了四个栅格翼。CMF上提供了通过CM-CES附件安装LEM、HEM、格栅翼及其展开机构和乘员模块的接口。

著录项

来源
《Current Science: A Fortnightly Journal of Research》 |2021年第1期|共12页
作者
Singh Nishant; Sajeev R. K.; Ayyappadas P.; Beena A. P.; Krishnadasan C. K.;
展开▼
作者单位

Vikram Sarabhai Space Ctr Struct Engn Ent Thiruvananthapuram 695022 Kerala India;

Vikram Sarabhai Space Ctr Struct Engn Ent Thiruvananthapuram 695022 Kerala India;

Vikram Sarabhai Space Ctr Struct Engn Ent Thiruvananthapuram 695022 Kerala India;

Vikram Sarabhai Space Ctr Struct Engn Ent Thiruvananthapuram 695022 Kerala India;

Vikram Sarabhai Space Ctr Struct Engn Ent Thiruvananthapuram 695022 Kerala India;

展开▼
收录信息
原文格式 PDF
正文语种 eng
中图分类自然科学现状及发展;
关键词
Aerodynamic stability; Crew Module Fairing; grid fins; Pat Abort Test;

机译：空气动力稳定性;船员舱整流罩;栅格鳍;Pat中止试验;

相似文献

外文文献
中文文献
专利

1. Applications of structural efficiency assessment method on structural-mechanical characteristics integrated design in aero-engines [J] . Jie HONG, Tianrang LI, Huaqiang ZHENG, 中国航空学报（英文版） . 2020,第004期
2. The Tank Design Bazaar Has Opened!--DHUB 2018SS Design Fair Has Kicked Off in Beijing [J] . Olivia Zhang 中国对外贸易：英文版 . 2017,第006期
3. Design optimization of first wall and breeder unit module size for the Indian HCCB blanket module [J] . Deepak SHARMA, Paritosh CHAUDHURI 等离子体科学和技术（英文版） . 2018,第006期
4. Model qualification of the PK-Sim (R) pediatric module for pediatric exposure assessment of CYP450 metabolized compounds [J] . Yun Yejin Esther, Edginton Andrea N. Journal of toxicology and environmental health, Part A . 2019,第13a18期

机译：用于CYP450代谢化合物的儿科暴露评估PK-SIM（R）儿科模块的模型资格
5. Stabilization of light-induced effects in Si modules for IEC 61215 design qualification [J] . Repins I. L., Kersten F., Hallam B., Solar Energy . 2020,第Sepa期

机译：IEC 61215设计资格的SI模块中光诱导效果的稳定化
6. A design and qualification of LED flip Chip-on-Board module with tunable color temperatures [J] . Fan Jiajie, Cao Jianwu, Yu Chaohua, Microelectronics & Reliability . 2018,第MAY期

机译：色温可调的LED倒装板上芯片模块的设计和鉴定
7. DESIGN, VERIFICATION AND GROUND QUALIFICATION APPROACH FOR THE STRUCTURE OF THE EUROPEAN SERVICE MODULE OF THE ORION MULTI-PURPOSE CREW VEHICLE [C] . Gandolfo DI VITA, Anthony C. THIRKETTLE, Paolo PALMIERI, International astronautical congress . 2016

机译：ORION多用途船员欧洲服务模块结构的设计，验证和地面资格方法
8. Evaluating fashion design information: The creation of assessment measures for the evaluation of fashion design using a MAL module to enhance fashion design information and analysis of fashion curriculum at a Taiwan university. [D] . Lin, Chia-Hsu. 2007

机译：评估时装设计信息：使用MAL模块创建评估时装设计的评估方法，以增强台湾大学的时装设计信息和时装课程分析。
9. What clinical crew competencies and qualifications are required for helicopter emergency medical services? A review of the literature [O] . Siobhán Masterson, Conor Deasy, Mark Doyle, 2020

机译：直升机紧急医疗服务需要哪些临床机组人员能力和资格？文献综述
10. STRUCTURAL DESIGN AND ANALYSIS OF THE UPPER PRESSURE SHELL SECTION OF A COMPOSITE CREW MODULE [O] . David W. Sleight, David Paddock, Jim Jeans, 2014

机译：复合船体模块上压壳结构设计与分析
11. Structural Element Testing in Support of the Design of the NASA Composite Crew Module. [R] . Kellas, S., Jackson, W. C., Thesken, J. C., 2012

机译：支持Nasa复合机组模块设计的结构单元测试。

Structural design, qualification and post-flight assessment of Crew Module Fairing

摘要

著录项

相似文献

相关主题

期刊订阅