Description:

TPA-SI are developing a new generation of nanosatellite platforms. There is an intention to develop in house CubeSat platform systems to be mounted to the external spacecraft structural walls to maximise payload volume. Moreover, a mission concept is in development for direct measurement of the lower thermosphere and upper mesosphere using aerodynamically stabilised “dart” satellites. These darts would b folded flat for deployment of a cluster of satellites which would deploy to their operational configuration. Such dart satellites could sample various atmospheric parameters, with an initial conceptual focus on Atomic Oxygen. There is therefore an opportunity to develop low profile avionics to address both needs, as well as the mechanical design of the darts and develop mission profile and science goals.

The project may consist of:

• Literature review of Lower thermosphere science with emphasis on Atomic Oxygen and state of the art in VLEO and disposable satellites
• Design of low profile spacecraft avionics
• Modelling of aerodynamic stabilisation
• Design and assembly of “pop-up” dart spacecraft
• Development of mission profile.

Details of emphasis of the research will be developed to address the student’s particular interests.

Type:

Undergraduate

Outcome:

Prerequisites

None

Specialisations

• Mechanical Engineering
• Mechatronics Engineering

Categories

• Design/Systems Engineering
• Mechatronics

Supervisor

• Benjamin Taylor

Team

• Shivam Desai
• Henissa Tong

Lab

Mechatronics Research (405.822, Lab)