6 results on '"Launchers"'
Search Results
2. Environmental life cycle assessment of reusable launch vehicle fleets: Large climate impact driven by rocket exhaust emissions.
- Author
-
Dominguez Calabuig, Guillermo J., Wilson, Andrew, Bi, Sifeng, Vasile, Massimiliano, Sippel, Martin, and Tajmar, Martin
- Subjects
- *
LAUNCH vehicles (Astronautics) , *PRODUCT life cycle assessment , *ROCKETS (Aeronautics) , *MOTOR vehicle driving , *RADIATIVE forcing - Abstract
After the success of the reusable Falcon 9 rocket, space actors are pursuing competitive space access by developing Reusable Launch Vehicles (RLVs). While this initiative may enhance recycling rates, it may also trigger the Jevons' paradox as it amplifies the overall environmental footprint due to increased launch frequencies. It is therefore essential to quantify RLVs' impacts and identify key design drivers to enable efficient design choices while mitigating undesirable environmental effects. Consequently, this article uses a space specific Life Cycle assessment (LCA) approach to evaluate the environmental footprint, in terms of climate impact, water depletion and land use, of different RLV fleets designed to serve a forecasted European space market. The results show that the LH 2 fleet options have 2–8 times lower carbon footprint when compared to the LCH 4 fleet as a result of lower propellant consumption and lack of black carbon emissions, suggesting that the environmental burdens are mostly driven by propellant choice. Moreover, the analysis reveals a potential underestimation of climate impacts in previous LCA's by 2–3 orders of magnitude due to the absence of high altitude characterisation of rocket exhaust emissions and demised aluminium oxides. This increased forcing could lead to fleet choices surpassing the Earth's carrying capacity given by its planetary boundaries. The methodology and results within this study can support further integration of launch and reentry emissions within LCA by refining modelling techniques, improving impact characterisation and quantifying uncertainties. These advancements can ultimately enable robust eco-design strategies for launch vehicles. • Life cycle assessment of launch vehicles including impacts from stratospheric radiative forcing. • Liquid hydrogen–oxygen fuelled fleets show lower impact than the liquid methane-oxygen fleet. • Global warming impacts in a 20 year horizon were 1.4–2.5 × higher than in a 100 year horizon. • Climate impacts become up to 1000 × higher when characterising high altitude emissions. • Impacts over the fleet lifetime comparable to annual emissions of global commercial aviation. [ABSTRACT FROM AUTHOR]
- Published
- 2024
- Full Text
- View/download PDF
3. Evaluating a Controlled Electromagnetic Launcher for Safe Remote Drug Delivery.
- Author
-
LaRocco, John, Tahmina, Qudsia, and Simonis, John
- Subjects
ELECTROMAGNETIC launchers ,AIR guns ,VETERINARY drugs ,KINETIC energy ,KINETIC control - Abstract
Biologists and veterinarians rely on dart projectors to inject animals with drugs, take biopsies from specimens, or inject tracking chips. Firearms, air guns, and other launchers are limited in their ability to precisely control the kinetic energy of a projectile, which can injure the animal if too high. In order to improve the safety of remote drug delivery, a lidar-modulated electromagnetic launcher and a soft drug delivery dart were prototyped. A single-stage revolver coilgun and soft dart were designed and tested at distances up to 8 m. With a coil efficiency of 2.25%, the launcher could consistently deliver a projectile at a controlled kinetic energy of 1.00 ± 0.006 J and an uncontrolled kinetic energy of 2.66 ± 0.076 J. Although modifications to charging time, sensors, and electronics could improve performance, our launcher performed at the required level at the necessary distances. The precision achieved with commercial components enables many other applications, from law enforcement to manufacturing. [ABSTRACT FROM AUTHOR]
- Published
- 2024
- Full Text
- View/download PDF
4. Evaluating a Controlled Electromagnetic Launcher for Safe Remote Drug Delivery
- Author
-
John LaRocco, Qudsia Tahmina, and John Simonis
- Subjects
coilgun ,launchers ,terminal ballistics ,motion control ,remote drug delivery ,Technology - Abstract
Biologists and veterinarians rely on dart projectors to inject animals with drugs, take biopsies from specimens, or inject tracking chips. Firearms, air guns, and other launchers are limited in their ability to precisely control the kinetic energy of a projectile, which can injure the animal if too high. In order to improve the safety of remote drug delivery, a lidar-modulated electromagnetic launcher and a soft drug delivery dart were prototyped. A single-stage revolver coilgun and soft dart were designed and tested at distances up to 8 m. With a coil efficiency of 2.25%, the launcher could consistently deliver a projectile at a controlled kinetic energy of 1.00 ± 0.006 J and an uncontrolled kinetic energy of 2.66 ± 0.076 J. Although modifications to charging time, sensors, and electronics could improve performance, our launcher performed at the required level at the necessary distances. The precision achieved with commercial components enables many other applications, from law enforcement to manufacturing.
- Published
- 2024
- Full Text
- View/download PDF
5. Geopolitics, the international dimension, and technology in Argentina and Brazil
- Author
-
Blinder, Daniel and Blinder, Daniel
- Abstract
The present work aims to enquire the space technology under a geopolitical point of view in Argentina and Brazil. Space technology is found in speeches of experts such as academics, technicians, journalists, military and politicians. I analyze the construction of space & technology regarding geopolitics associated to a geopolitical Great Game in which artifacts and technology knowledge play a central role as a technopolitical instrument of power. I present and review technolopolitical speeches made by presidents of both States regardig space policy., El presente trabajo tiene por objetivo indagar desde una perspectiva geopolítica la cuestión tecnológica a partir de los casos de la tecnología espacial en la República Argentina y la República Federativa del Brasil. La tecnología espacial ha estado vinculada en los discursos de los llamados expertos, académicos, técnicos, periodistas, militares y políticos a la política internacional, e inmediatamente asociada como sinónimo a geopolítica, implicando un Gran Juego en el cual el artefacto y saber tecnológico juega un rol central como instrumento en las relaciones de poder. Analizaremos críticamente esta idea, criticando la construcción de la idea de tecnología como instrumento tecnopolítico de poder. Se abordará e indagará tanto la tecnopolítica como los discursos geopolíticos presidenciales sobre la política espacial argentina y brasilera., O presente trabalho tem como objetivo investigar a tecnologia espacial do ponto de vista geopolítico na Argentina e no Brasil. A tecnologia espacial é encontrada em discursos de especialistas como acadêmicos, técnicos, jornalistas, militares e políticos. Analiso a construção do espaço e da tecnologia no que se refere à geopolítica associada a um Grande Jogo geopolítico em que artefatos e conhecimento tecnológico desempenham um papel central como instrumento tecnopolítico de poder. Apresento e reviso discursos tecnolopolíticos proferidos por presidentes de ambos os Estados a respeito da política espacial.
- Published
- 2023
6. Emission-Driven Hybrid Rocket Engine Optimization for Small Launchers
- Author
-
Filippo Masseni, Lorenzo Casalino, Dario Pastrone, and Andrea Ferrero
- Subjects
Access to space ,Launchers ,hybrid rocket engines ,multidisciplinary optimization ,green propulsion ,Emission-driven optimization ,Small launchers ,Aerospace Engineering - Abstract
Hybrid rocket engines are a green alternative to solid rocket motors and may represent a low-cost alternative to kerosene fueled rockets, while granting performance and control features similar to that of typical storable liquid rocket engines. In this work, the design of a three-stage hybrid launcher is optimized by means of a coupled procedure: an evolutionary algorithm optimizes the engine design, whereas an indirect optimization method optimizes the corresponding ascent trajectory. The trajectory integration also provides the vertical emission profiles required for the evaluation of the environmental impact of the launch. The propellants are a paraffin-based wax and liquid oxygen. The vehicle is launched from the ground and uses an electric turbo pump feed system. The initial mass is given (5000 kg) and the insertion of the payload into a 600-km circular, and polar orbit is considered as a reference mission. Clusters of similar hybrid rocket engines, with only few differences, are employed in all stages to reduce the development and operational costs of the launcher. Optimization is carried out with the aim of maximizing the payload mass and then minimizing the overall environmental impact of the launch. The results show that satisfactory performance is achievable also considering rocket polluting emissions: the carbon footprint of the launch can be reduced by one fourth at the cost of a 5-kg payload mass reduction.
- Published
- 2022
- Full Text
- View/download PDF
Catalog
Discovery Service for Jio Institute Digital Library
For full access to our library's resources, please sign in.