Eco-design of future reusable launchers: insight into their life-cycle and atmospheric impact

GJ Dominguez Calabuig, L Miraux, AR Wilson… - Proceedings of the 9th …, 2022 - arpi.unipi.it
Reusable launch vehicles (RLV) are slowly emerging as a solution to reduce space access
costs, bring ing potential benefits from novel breakthrough space application. Whilst space …

[图书][B] Radiative heat transfer in turbulent combustion systems: theory and applications

MF Modest, DC Haworth - 2016 - books.google.com
This introduction reviews why combustion and radiation are important, as well as the
technical challenges posed by radiation. Emphasis is on interactions among turbulence …

Heat transfer—a review of 2002 literature

RJ Goldstein, ERG Eckert, WE Ibele… - International Journal of …, 2005 - Elsevier
Heat transfer continues to be a field of major interest to engineering and scientific
researchers, as well as designers, developers, and manufacturers. Considerable effort has …

The climate and ozone impacts of black carbon emissions from global rocket launches

CM Maloney, RW Portmann, MN Ross… - Journal of …, 2022 - Wiley Online Library
Aerosol emissions from spaceflight activities play a small but increasing role in the
background stratospheric aerosol population. Rockets used by the global launch industry …

Investigating the rocket base flow characteristics and thermal environment of different nozzle configurations considering afterburning

Z Zhou, Y Bao - International Journal of Thermal Sciences, 2023 - Elsevier
During launch vehicle ascent, the base flow regimes of multi-nozzle rockets become
increasingly complex owing to plume interactions. We developed a numerical method using …

Numerical analysis of point-source infrared radiation phenomena of rocket exhaust plumes at low and middle altitudes

Q Niu, X Duan, X Meng, Z He, S Dong - Infrared Physics & Technology, 2019 - Elsevier
Rocket exhaust plume treated as a significant radiation source has been widely used in
space-based detection. In this paper, infrared radiation signatures of plumes were studied in …

[HTML][HTML] A numerical study on the influence of multiple nozzles on the infrared radiation signatures of liquid rocket exhaust plumes

P Yan, W Gao, X Meng, H Wang, Q Niu… - Case Studies in Thermal …, 2024 - Elsevier
A numerical study was conducted to examine the relationship between the infrared radiation
characteristics of liquid rocket engine exhaust plumes under the same thrust conditions and …

Experimental and numerical study on the combustion and infrared radiation characteristics of Mg/PTFE/Viton pyrotechnic compositions

K Zhang, D Ren, Y Han, C Zhu - Infrared Physics & Technology, 2023 - Elsevier
The combustion process of Mg/PTFE/Viton-based pyrotechnics exhibits a complex
multiphase flow phenomenon. However, the influence mechanism of metal particles …

Infrared signature of NEPE, HTPB rocket plume under varying flight conditions and motor size

S Kim, S Kim, M Kim, S Song, JS Lee - Infrared Physics & Technology, 2021 - Elsevier
In this study, radiation signatures of rocket plumes based on HTPB and NEPE propellants
are simulated under varying altitudes, flight Mach numbers, and motor size. The flow field of …

A simplified model for fast estimating infrared thermal radiation of low-altitude under-expanded exhaust plumes

Q Niu, D Fu, S Dong, H Tan - International Journal of Heat and Mass …, 2019 - Elsevier
In this paper, a fast estimating method of thermal infrared radiation signatures for low-
altitude exhaust plumes was proposed. In engineering application, it is essential to predict …