Starworks - Southampton University Spaceflight Society

Starworks

Our Starworks project is developing a propulsive self-landing vehicle to be one of a few teams within Europe to compete in the Collegiate Lander Challenge

What is VTVL?

VTVL (Vertical Take-off; Vertical Landing) describes a launch system which has the capabilities to take off - as all functional rockets do - and also land - which very few do. The key advantage of a VTVL compared to an ordinary launch vehicle is that it can be reused and reflown.

As Falcon 9 has shown, this single advantage can change the face of the space industry: it reduces launch costs, increases launch frequency, improves sustainability and supports future space operations. For SUSF it allows us to develop the skills to engage with this forefront of this space industry - as well as for general lander technology, which has many similarities.

There are significant engineering challenges, or significant opportunities to our Starworks team. An example is the guidance and navigation subsystems, which must both be complex and adaptable. The engine must also be capable of being very throttleable and reusable, whilst the entire structure must withstand a range of thermal and structural loads. Overall this makes VTVL very difficult, but there benefits on modern spaceflight are significant, and for deeper space exploration: vital.

Starworks Mission

Starworks mission is to design a fully functional VTVL vehicle and test fly it! This is a very complex multi stage aim, with many engineering considerations and components. Because of this, Starworks is aiming to compete in the American Collegiate Propulsive Landing Challenge (CPLC) and follow their framework and design goals. This sets clear requirements for Starworks to achieve and stages for the project to work through whilst rewarding Starworks financially for significant progress.

Beyond this, Starworks will continue to improve its VTVL technology above the limitations of this specific competition.

Starworks Mission Profile

01

TVC Hotfire

Static fire of a thrust-vector-controlled liquid engine — gimbal alignment plus a sustained hot fire

02

Throtteable Engine Hotfire

Static fire of a throttleable liquid engine — variable thrust under closed-loop control

03

Tethered Hover

$25,000

Stable, controlled hover on a tethered vehicle for a sustained duration

04

The Bess

Touchdown Award

$25,000

Precision landing on the designated target with a controlled descent profile

05

Hop

$50,000

A full ascent, translation, and propulsive landing — all subsystems integrated

Starworks

Propulsion

(1) Banshee regeneratively cooled subsystem

(2) Banshee throttle-capable feed subsystem

(3) Collaborate with hardware sub-team on thrust vector control subsystem

Hardware

(1) Develop Guidance, Navigation and Control subsystem's hardware

(2) Design the Thrust Vectoring hardware alongside the propulsion sub-team

(3) Develop test stand and hardware

Software

(1) Develop Guidance, Navigation and Control subsystem's software

(2) Design guidance algorithms, attitude control, and trajectory prediction systems

Structures

(1) Develop Banshee to vehicle adapter

(2) Develop landing legs

(3) Develop fuel system interface

(4) Develop overall vehicle structure

Michal Rado

Propulsion Lead

Liquid Bipropellant Engine: tanks, feed, test.

Michal_Crowdfunder

Adel Patell

Hardware Lead

TVC for landing burn, ACS systems.

Starworks logo

Adi Soundalgekar

Software Lead

Embedded flight computer, sensors, telemetry.

MG_92991

William Patey

Structures Lead

Main body, integration.

Starworks logo

Diego Paniagua Silva

Project Lead

Diego_Project-Head