首页> 美国政府科技报告 >Parametric Mass Modeling for Mars Entry, Descent and Landing System Analysis Study

【24h】

Parametric Mass Modeling for Mars Entry, Descent and Landing System Analysis Study

机译：火星进入，下降和着陆系统分析研究的参数化质量模型

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

This paper provides an overview of the parametric mass models used for the Entry, Descent, and Landing Systems Analysis study conducted by NASA in FY2009-2010. The study examined eight unique exploration class architectures that included elements such as a rigid mid-L/D aeroshell, a lifting hypersonic inflatable decelerator, a drag supersonic inflatable decelerator, a lifting supersonic inflatable decelerator implemented with a skirt, and subsonic/supersonic retro-propulsion. Parametric models used in this study relate the component mass to vehicle dimensions and mission key environmental parameters such as maximum deceleration and total heat load. The use of a parametric mass model allows the simultaneous optimization of trajectory and mass sizing parameters.

著录项

作者
Samareh, J. A.; Komar, D. R.;
展开▼
作者单位

展开▼
年度 2011
页码 1-16
总页数 16
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Descent ; Landing aids ; Systems analysis ; Aerodynamic brakes ; Mars landing ; Supersonic flight ; Drag ; Deceleration ; Loads(Forces) ; Propulsion ; Trajectories;

机译：下降;着陆辅助系统;系统分析;空气动力制动;火星着陆;超音速飞行;阻力;减速;载荷（力）;推进;轨迹;

相似文献

外文文献
中文文献
专利

1. Entry descent and landing systems for small planetary missions: Parametric comparison of parachutes and inflatable systems for the proposed Vanguard Mars mission [J] . E. Allouis, A. Ellery, C.S. Welch Acta astronautica . 2006,第8a11期

机译：小型行星飞行任务的入口下降和着陆系统：拟议的Vanguard Mars飞行任务的降落伞和充气系统的参数比较
2. Mars Phoenix Entry, Descent, and Landing Simulation Design and Modeling Analysis [J] . Jill L. Prince, Prasun N. Desai, Eric M. Queen, Journal of Spacecraft and Rockets . 2011,第5期

机译：火星凤凰号进入，下降和着陆仿真设计与建模分析
3. A concept for the entry, descent, and landing of high-mass payloads at Mars [J] . Ashley M. Korzun, Gregory F. Dubos, Curtis K. Iwata, Acta astronautica . 2010,第7a8期

机译：高质量载荷在火星上的进入，下降和着陆的概念
4. Parametric Mass Modeling for Mars Entry, Descent and Landing System Analysis Study [C] . Jamshid A. Samareh, D. R. Komar AIAA aerospace sciences meeting including the new horizons forum and aerospace exposition . 2011

机译：火星进入，下降和着陆系统分析研究的参数质量建模
5. A Systems and Cost Analysis of Human Rated Mars Entry, Descent, and Landing Vehicles [D] . Friz, Paul Daniel. 2019

机译：人类额定火星入口，下降和降落车辆的系统和成本分析
6. A Novel Mass-Spring-Damper Model Analysis to Identify Landing Deficits in Athletes Returning to Sport after ACL Reconstruction [O] . Daniel K. Schneider, Alli Gokeler, Bert Otten, -1

机译：一种新颖的质量弹簧阻尼器模型分析用于识别ACL重建后重返运动场的运动员的着陆缺陷
7. Parametric Mass Modeling for Mars Entry, Descent and Landing System Analysis Study [O] . Samareh Jamshid A., Komar D. R. 2011

机译：火星进入，下降和着陆系统分析研究的参数质量建模

Parametric Mass Modeling for Mars Entry, Descent and Landing System Analysis Study

摘要

著录项

相似文献

相关主题

期刊订阅