Aerospace Engineering is a field that focuses on the design, development, testing, and production of air and spacecraft. This includes aircraft, satellites, missiles, and launch vehicles. Aerospace Engineers must possess a unique combination of critical thinking and problem-solving skills to create safe, effective, and economical designs. With the help of our skilled Aerospace Engineers, clients can build equipment that can operate amidst tremendous atmospheric stresses and forces.
Here's some projects that our expert Aerospace Engineers have made real:
- Simulations of real-world mechanics
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- Analysis of airflows over components
- Optimization of aerospace components
- Modelling of space station design
- Development of CAD models for sounding rockets
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- Calculation of wind forces on inclined cylinders
- Evaluation of domestic innovation in aircrafts in China from various eras
- Airfoil analysis using advanced tools such as QBlade.
Our Aerospace Engineers are experienced in a broad range of areas, allowing them to leverage their knowledge and experience to help our clients solve complex tasks related to Aerospace Engineering. If you have a project that requires an experienced Aerospace Engineer then post it now on Freelancer.com and get the help you need today.From 9,302 reviews, clients rate our Aerospace Engineers 4.78 out of 5 stars.
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I’m currently trying to work on a code to calculate trajectories for rapid response missions to NEO’s. (Preferably from a parked earth orbit to a “moving” NEO) I want the code to consider NEO characteristics, orbital mechanics & collision detection. As well as show some sort of diagram to “view” the trajectory calculated. Basically need it to calculate the trajectory view, delta V, time to collision, impact point, risk level and any other necessary value you can think of It also needs to include the following: - NEO classification criteria ( into high, moderate and low risk based on size, speed) - Impact energy thresholds - Easy to input parameters I currently have a few files of code that I can send that it sort of needs to be based on Key po...
ELO2 Big Dipper Lunar Regolith Acquisition Phase 2 Challenge Phase 2 Welcome to Phase 2 of the Big Dipper Lunar Regolith Acquisition Challenge! Whether you participated in Phase 1 or are just entering the competition now, we’re thrilled to have you on-board! Phase 2 of this challenge, open to existing and new solvers, offers a unique opportunity to build upon the achievements of Phase 1 and further contribute to the success of this ground-breaking Australian rover design. This phase will seek submissions that concisely summarise unique and creative insights drawn from the winning solutions, judges’ feedback, open testing, and your own research in a visually appealing way. Submissions will be in the form of a one-page infographic illustrating insights and design recommendatio...
Participants need to fill out the Challenge Registration form before submitting the solution. Please refer to the Guidelines tab for more information. Overview As space travel extends to greater duration and distance, missions may require a propellant refill in space. To achieve this, spacecraft may require larger tanks and efficient refueling along with tanks that have the capability of isolating propellant from ullage fluid (a gas and vapor mixture) during a vent. The goal of this Challenge is to develop a novel solution for the venting of ullage contents from a partially full propellant tank, in microgravity, with minimal loss of propellant. This ullage venting solution would help allow the adjustment of pressure in the receiving tank prior to, during, and/or after the liquid propella...