The Nexus Aurora Spaceshot project aims to achieve a visible technical milestone by developing a small launch vehicle, engaging university teams, and creating a reusable commercializable rocket platform.
- General Vehicle Details:
- The vehicle is designed by the university team to carry a 5 kg Nexus Aurora payload to the target altitude and ensure safe recovery and reuse.
- The vehicle must have the capability to determine and transmit its location and flight characteristics back to the ground team.
- Projected Altitude:
- Baseline performance targets include reaching an altitude of 130-180 km and achieving approximately 4 minutes of microgravity exposure.
- Projected Recovery System:
- The recovery system is to be defined and developed by the university team, with an emphasis on ensuring complete reusability and safe landing.
- Project Propulsion:
- MARS Aerospace provides propulsion systems according to the university team’s requirements, with solid rocket motors capable of meeting altitude and performance specifications.
- Project Payload:
- Nexus Aurora will seek commercial partnerships to develop, manufacture, and test custom payloads, offering flight opportunities for research and technology validation in high-altitude environments.
Team
- The team is structured into Integrated Product Teams (IPTs) managed by a Project Manager and Chief Engineer, ensuring efficient coordination and execution.
- Universities are invited to participate by submitting technical proposals, contributing to vehicle design, and collaborating on various aspects of the project.
Project Milestones
- Team Solicitations and Selection: Winter 2025
- Preliminary Design Review: Summer 2026
- Critical Design Review: Winter 2026
- Flight Readiness Review: Winter 2027
- Launch Campaign: Summer 2028
