Structural reliability evaluation is critical for mission planning of reusable spacecraft. A dynamic reliability prognosis method based on digital twin framework is proposed for mission planning in this work. https://lnkd.in/gb4xuYkp

The Purpose Of Reaction Control Systems On Spacecraft Learn more and read the full, in-depth article by following the link below: https://lnkd.in/d_4U3Y5G

Pulsed plasma rocket (PPR): Shielded, fast transits for humans to Mars, Credit: Pixabay/CC0 Public Domain The future of a space-faring civilization will depend on the ability to move both cargo and humans efficiently and rapidly. Due to the extremely large distances that are involved in space travel, the spacecraft must reach high velocities for reasonable mission transit times. Thus, a propulsion system that produces a high thrust with a high specific impulse is essential. However, no such technologies are

Incrivel!!! This image shows the results of a lab test impact between a small sphere of aluminum travelling at approximately 6.8 km/second and a block of aluminum 18 cm thick. This test simulates what can happen when a small space debris object hits a spacecraft. Al sphere diameter: 1.2cm Al sphere mass: about 1.7 g Impact crater diameter: 9.0 cm Impact crater depth: 5.3 cm In such an impact, the pressure and temperature can exceed those found at the centre of the Earth, e.g. greater than 365 GPa and more than 6000 K. https://lnkd.in/ehFeUC6g

New Post: Pulsed Plasma Rocket (PPR): Shielded, Fast Transits for Humans to Mars - https://lnkd.in/emKR5gMS ClementsHowe Industries The future of a space-faring civilization will depend on the ability to move both cargo and humans efficiently and rapidly. Due to the extremely large distances that are involved in space travel, the spacecraft must reach high velocities for reasonable mission transit times. Thus, a propulsion system that produces a high thrust […]

How do Shockwaves form around a re-entry capsule on MARS? Check out this simulation video of a reentry capsule entering Mars' atmosphere. In this video it is shown how the flow of air around the capsule changes at different angles as it travels at supersonic speeds. By adjusting the angle of attack, we can see how shockwaves and vortices form around the capsule. The simulation uses LES (Large Eddy Simulation). This helps us in understanding what happens during reentry. This data can be further used in designing safe and efficient spacecraft. Source : https://lnkd.in/d9CaRaHa ♻️ Repost if you find this post interesting. __________________________________________________________ Want to stay connected? Follow me Sarah Mirza and click the 🔔 to stay informed!

New Post: Pulsed Plasma Rocket (PPR): Shielded, Fast Transits for Humans to Mars - https://lnkd.in/eHMMcS8B ClementsHowe Industries The future of a space-faring civilization will depend on the ability to move both cargo and humans efficiently and rapidly. Due to the extremely large distances that are involved in space travel, the spacecraft must reach high velocities for reasonable mission transit times. Thus, a propulsion system that produces a high thrust […]

New Post: Pulsed Plasma Rocket (PPR): Shielded, Fast Transits for Humans to Mars - https://lnkd.in/eHMMcS8B ClementsHowe Industries The future of a space-faring civilization will depend on the ability to move both cargo and humans efficiently and rapidly. Due to the extremely large distances that are involved in space travel, the spacecraft must reach high velocities for reasonable mission transit times. Thus, a propulsion system that produces a high thrust […]

To a galaxy far, far away! Embarking on a journey through space demands precision and innovation. In this case study, we delve into the intricacies of spacecraft re-entry into the Mars atmosphere, comparing numerical methods with real data from the Viking reentry capsule. Download now for key findings: https://lnkd.in/eW7kXQEh #aerospaceengineering #meshing #spaceexploration