Jun 24, 2019 · A new design for a blunt re-entry craft, with no parachute and a crushable front shield, has been developed and designed for the Marco Polo mission. The mission plans to return a sample …

Jul 23, 2024 · Thus, all design requirements were satisfied, ensuring thermal protection performance and structural safety. The thermal–structural coupled analysis and design procedure proposed in this …

Apr 19, 2017 · The purpose of this article is to improve the computational performance of algorithms for multi-module or supporting surface satellite module component layout optimization. The proposed …

As the IXV precursor was, the re-entry module itself is a test bed for entry technologies. The project is currently running Phase C heading towards Critical Design Review (CDR) by the end of the year. …

Jul 1, 2019 · The design presented in this work successfully passed the Critical Design Review of the Space Rider guidance, navigation, and control subsystem in December 2019.

The Dragon spacecraft design is structurally identical for both cargo and crewconfigurations. With a nominal internal or ex ternal cargo mass of 2550 kg of cargo, Dragon has a gross liftoff weight of …

The Crew Module Atmospheric Re-entry Experiment (CARE) is an experimental test vehicle for the Indian Space Research Organisation 's future ISRO orbital vehicle called Gaganyaan. [1] It was …

The Apollo command module was the first manned spacecraft to be designed to enter the atmos- phere of the earth at lunar-return velocity, and the design of the thermal protection subsystem for the …

Crew Module including validating the performance of parachute based deceleration system. CARE is expected to enhance the understanding of blunt body re-entry aerothermodynamics and parachute …

Feb 29, 2024 · Explore re-entry heat shields, their advanced materials, and designs that protect spacecraft during fiery atmospheric returns.