Conceptual design analysis for a two-stage-to-orbit semi-reusable launch system for small satellites-Reference-Cited by-同舟云学术

Conceptual design analysis for a two-stage-to-orbit semi-reusable launch system for small satellites

Published:2018-11 Issue: Volume:152 Page:782-792
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Maddock Christie Alisa^ORCID,Ricciardi Lorenzo^ORCID,West Michael,West Joanne,Kontis Konstantinos,Rengarajan Sriram,Evans David,Milne Andy,McIntyre Stuart

Funder

UK Space Agency

National Space Technology Programme (NSTP) Sub-Orbital and Small Launcher Research Projects

European Space Agency General Support Technology Programme

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference32 articles.

1. How to launch small payloads? evaluation of current and future small payload launch systems;Maddock,2016

2. 2017 nano/microsatellite Market Forecast;Doncaster,2017

3. Global space industry: refining the definition of new space;Hay,2009

4. Small launch vehicles– a 2015 state of the industry survey;Niederstrasser,2015

5. Stagewise multidisciplinary design optimization formulation for optimal design of expendable launch vehicles;Balesdent;J. Spacecraft Rockets,2012

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Derivation and validation of a similarity law for free-flight wind tunnel tests of parallel stage separation;Chinese Journal of Aeronautics;2023-08

2. Multistage rocket preliminary design and trajectory optimization using a multidisciplinary approach;Structural and Multidisciplinary Optimization;2022-06-28

3. Multi-Objective Optimisation under Uncertainty with Unscented Temporal Finite Elements;Mathematics;2021-11-24

4. Longitudinal aerodynamic modeling and verification for air-launch-to-orbit system during stage separation;Aerospace Science and Technology;2021-10

5. Robust Trajectory Optimisation of a TSTO Spaceplane Using Uncertainty-Based Atmospheric Models;23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2020-03-10