A flexible multi-disciplinary environment for performance, life-cycle cost, and safety evaluation of suborbital vehicles-Reference-Cited by-同舟云学术

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A flexible multi-disciplinary environment for performance, life-cycle cost, and safety evaluation of suborbital vehicles

Published:2018-06 Issue: Volume:77 Page:555-562
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Frank Christopher P.^ORCID,Pinon-Fischer Olivia J.,Mavris Dimitri N.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference47 articles.

1. Flight mechanics of manned sub-orbital reusable launch vehicles with recommendations for launch and recovery;Sarigul-Klijn,2003

2. Design sheet: an environment for facilitating flexible trade studies during conceptual design;Buckley,1992

3. A trajectory synthesis simulation program for the conceptual design of a suborbital tourism vehicle;Huang,2005

4. Aircraft Engine Design;Mattingly,2002

5. T. Nam, Introduction to FLOPS modeling, University Lecture, 2012.

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1. Design optimization of a low-cost three-stage launch vehicle with modular hybrid rocket motors;Journal of Physics: Conference Series;2024-05-01

2. Thermomechanical Behaviors of a Novel Double-Layer Corrugated Core Structure for Thermal Protection System;International Journal of Aerospace Engineering;2023-07-17

3. A self-adaptive local diversity-preserving NSGA-II for the multidisciplinary design optimization of a miniaturized supersonic rocket;Aerospace Science and Technology;2023-05

4. Multi-Objective, Multi-Disciplinary Design Optimization and Multi-Attribute Evaluation of Hybrid Rocket Motors Used for Manned Lunar Lander;Aerospace;2023-03-10

5. A Modular Framework for the Life Cycle Based Evaluation of Aircraft Technologies, Maintenance Strategies, and Operational Decision Making Using Discrete Event Simulation;Aerospace;2021-07-14

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