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This paper presents three case studies of educators pioneering transdisciplinary project work within a UK College-Based Higher Education Institution, focusing on Education Studies, Counselling, and Fine Art. Through the CollaborArt Blackburn initiative, educators facilitated gallery visits, encounter spaces, and collaborative creation opportunities for students across these disciplines. These case studies highlight the educators' roles in fostering a transdisciplinary approach that transcends traditional disciplinary boundaries, emphasising experiential learning and collaborative engagement. The narratives illustrate the transformative impact of integrating diverse perspectives and methodologies, enriching both educators' and students' understanding and practice. The paper argues for the intrinsic value of educators' insights and expertise in initiating and sustaining transdisciplinary projects, encouraging peers to embrace innovative approaches in their pedagogical practices. This work contributes to the discourse on transdisciplinary education, advocating for its potential to create dynamic, inclusive, and holistic learning environments.

Rotating (also termed continuous spin) detonation technology is gaining interest in the global research and development community due to the potential for increased performance. Potential performance benefits, thrust chamber design, and thrust chamber cooling loads are analyzed for propellant applications using liquid oxygen or high-concentration hydrogen peroxide oxidizers with kerosene, hydrogen, and methane fuels. Performance results based on a lumped parameter treatment show that theoretical specific impulse gains of 3–14% are achievable with the highest benefit coming from hydrogen-fueled systems. Assessment of thrust chamber designs for notional space missions shows that both thrust chamber length and diameter benefits are achievable given the tiny annular chamber volume associated with the rotating detonation combustion. While the passing detonation front drastically increases local heat fluxes, global energy balances can be achieved if operating pressures are limited to be comparable to existing or prior space engines.