Safety-guided design & analysis of space launch vehicles by Rising, John M. (John Michael)

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Systems-Theoretic Process Analysis of space launch vehicles by Rising, John M., Leveson, Nancy G

“…This article reviews safety analysis methods as they are applied to space launch vehicles, and demonstrates that they are unable to treat many of the causal factors associated with modern launch accidents. …”
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Developing a component reuse strategy for space launch vehicles by Good, Marissa Ann

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A framework for safe system design in space launch vehicles by Schlegelmilch, Barret William

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Rapid Evaluation of the Destructive Power Caused by Accidental Explosion of Space Launch Vehicles by Liangliang Ding, Xiaoxiao Cui, Liancheng Lu, Xufeng Yin, Xiaoguang Xue, Yuli Zhao, Xu Zhou

Subjects: “…space launch vehicles…”
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Application of Novel Additive Manufacturing Techniques for Cost Reduction in Space Launch Vehicles by Johanson, Robert T.

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Real-Time Trajectory Estimation of Space Launch Vehicle Using Extended Kalman Filter and Unscented Kalman Filter by Jeong-Ho Baek, Sang-Young Park, Eun-Seo Park, Kyu-Hong Choi, Hyung-Chul Lim, Jong-Uk Park

“…This research supposed when a fictitious KSLV-I space launch vehicle launches from NARO space center. This compared and analyzed the results from real-time trajectory estimation using the Extended Kalman Filter and the Unscented Kalman Filter. …”
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Development of Solid Gas Generating Compositions to Ensure Non Explosiveness of Spent Orbital Stages of Liquid Rocket of Space Launch Vehicles by V. I. Trushlyakov, K. I. Zharikov, D. B. Lempert

“…The choice is discussed of solid gas generating compositions for venting by hot combustion products a fuel tank of the spent orbital stage of a space launch vehicle with a main liquid rocket engine. Non explosiveness is achieved via eliminating the possibility of freezing the drainage system when products of gasification (vapours of a propellant component + the remains of a gas boost + the hot products of combustion of solid gas generating compositions) are discharged from the tank into surrounding space. …”
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Ground Contact Analysis for Korea’s Fictitious Lunar Orbiter Mission by Young-Joo Song, Sang-il Ahn, Su-Jin Choi, Eun-Sup Sim

Subjects: “…INTRODUCTION Since the successful launch of Korea Space Launch Vehicle–I (KSLV–I) on Jan. 30…”
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Dynamics and simulation of flexible rockets / by Barrows, Timothy M., author 650757, Orr, Jeb S., author 650758, ScienceDirect (Online service) 7722

“…The book also discusses important forms of coupling, such as between the nozzle motions and the flexible body.This book is designed to help practicing aerospace engineers create simulations that can accurately verify that a space launch vehicle will successfully perform its mission. …”
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A Liquid Launch Vehicle Safety Assessment Model Based on Semi-Quantitative Interval Belief Rule Base by Xiaoyu Cheng, Guangyu Qian, Wei He, Guohui Zhou

“…As the propulsion part of a space launch vehicle and nuclear weapon missile, the health status of the liquid rocket determines whether the space launch vehicle and nuclear weapon missile can function normally. …”
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Recent and Future Development of Space Exploration (Development and Applications) / by Chadwick, Nicola, author 648392

“…Iraq developed and tested the Tammouz space launch vehicle without a satellite on 5 December 1989. …”
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Distributed multiple model extended information filter with unbiased mixing for satellite launch vehicle tracking by Haryong Song, Yongtae Choi

“…We prove the superiority of the proposed algorithm by conducting Monte Carlo simulation with nominal trajectory data of Korea Space Launch Vehicle-1. Comparative simulation results demonstrate that the performance of the proposed method has been improved in vehicle’s position root mean square error.…”
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Energetic Compositions Application for the Reduction of the Environmental Pollution Because of Space Vehicle Launches by V. Trushlyakov, D. Lempert, Yuan- jie Shu

“…This technogeneous impact is not only the pollution of near Earth space with space debris (worked-off stages of space launch vehicle (SLV)), but also the pollution of significant areas on the Earth surface with worked-off lower stages of SLV, which fall down after having accomplished their mission. …”
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Numerical and Experimental Study of Nose for LOx Floating Ring Seal in Turbopump by Joon-Hwan Bae, Hyun-Duck Kwak, Sung-Jae Heo, Chang-Ho Choi, Jong-Soo Choi

“…The oxidizer pump of the 7 tonf liquid engine in the Korea Space Launch Vehicle II (KSLV-II) operates at high rotational speeds and under cryogenic conditions and has floating ring seals in the bearing cooling path to reduce leakages. …”
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Environmental Impact of Space Launches and Societal Response by Sirieys, Elwyn

“…A historical analysis of space launch vehicle designs is conducted, based on a comprehensive record of 6,502 orbital launches for the period 1957-2021, to inform on technological evolution and implications in terms of emissions. …”
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Science Objectives and Design of Ionospheric Monitoring Instrument Ionospheric Anomaly Monitoring by Magnetometer And Plasmaprobe (IAMMAP) for the CAS500-3 Satellite by Kwangsun Ryu, Seunguk Lee, Chang Ho Woo, Junchan Lee, Eunjin Jang, Jaemin Hwang, Jin-Kyu Kim, Wonho Cha, Dong-guk Kim, BonJu Koo, SeongOg Park, Dooyoung Choi, Cheong Rim Choi

“…The Ionospheric Anomaly Monitoring by Magnetometer And Plasma-probe (IAMMAP) is one of the scientific instruments for the Compact Advanced Satellite 500-3 (CAS 500-3) which is planned to be launched by Korean Space Launch Vehicle in 2024. The main scientific objective of IAMMAP is to understand the complicated correlation between the equatorial electro-jet (EEJ) and the equatorial ionization anomaly (EIA) which play important roles in the dynamics of the ionospheric plasma in the dayside equator region. …”
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Korean Mars Mission Design Using KSLV-III by Young-Joo Song, Sung-Moon Yoo, Eun-Seo Park, Sang-Young Park, Kyu-Hong Choi, Jae-Cheol Yoon, Jo Ryeong Yim, Joon-Min Choi, Byung-Kyo Kim

“…Mission opportunities and trajectory characteristics for the future Korean Mars mission have designed and analyzed using KSLV-III(Korea Space Launch Vehicle-III). Korea's first space center, ``NARO space center'' is selected as a launch site. …”
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Design and Testing of an Adaptive In-phase Magnetometer (AIMAG), the Equatorial-Electrojet-Detecting Fluxgate Magnetometer, for the CAS500-3 Satellite by Seunguk Lee, Kwangsun Ryu, Dooyoung Choi, Seongog Park, Jinkyu Kim, Wonho Cha, Bonju Gu, Jimin Hong, Suhwan Park, Eunjin Jang, Cheongrim Choi, Daeyoung Lee

“…Ionospheric Anomaly Monitoring by Magnetometer And Plasma-probe (IAMMAP) is a suite of scientific instruments used in the Compact Advanced Satellite 500-3 (CAS 500-3), which is planned to be launched by the KSLV (Korean Space Launch Vehicle) in 2025. The main scientific objective of IAMMAP is to understand the complicated correlation between the equatorial electrojet (EEJ) and the equatorial ionization anomaly (EIA), both of which play important roles in the dynamics of ionospheric plasma in the dayside equator region. …”
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Structural Health Monitoring of Solid Rocket Motors: From Destructive Testing to Perspectives of Photonic-Based Sensing by Georgia Korompili, Günter Mußbach, Christos Riziotis

“…Serving as boosters in space launch vehicles and employed in military systems, and other critical & emerging applications, SRMs’ structural integrity monitoring, is of paramount importance. …”
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