Resilient Mobile Space Launch System

Background

There is only one geographically relevant polar launch site in the US which is in danger of being unavailable during times of conflict. This project would create the first road-mobile launch system that can launch a payload to a polar orbit to remedy this problem.

Goal and Objectives

We will develop a conceptual design for a TEL (transporter, erector, and launcher) and a launch vehicle. The TEL will transport, erect, and launch the launch vehicle, and will follow standard Department of Transportation requirements so it can operate on standard US highways and roads. It will also hold down the launch vehicle at 100% thrust level before release and can be set up within 8 hours of arrival at the launch site. The launch vehicle will be capable of launching a 200 lb payload to a 500 km, sun-synchronous polar orbit and will have a reusable first stage. It will also utilize existing LOX/hydrocarbon engines. The final project objectives are to create a conceptual CAD design for the entire system and verify the launch vehicle design through simulation. A physical representation of the TEL using additive manufacturing and scaled-down mechanics will also be created by the end.

The Problem Definition Presentation was completed on February 4, 2025, and the Preliminary Design Review was completed on February 13, 2025. 

The launch vehicle will have its dimensions and thrust finalized, as well as a proof of concept simulation run using our sponsor’s software by March 14, 2025.

The TEL team will have a scaled-down model of the erector using proper hydraulics by March 14, 2025.

Documentation

https://drive.google.com/drive/folders/1-AVx0WY_synr7wYe7QlsczO7zYDOOjVx?usp=sharing

Team Contact

Natalie Ang, angns@uci.edu

Sponsor/Advisor

Jeff Lane, jlane@vector-launch.com