Novel Drop Test Set-Up For Hypergolic Testing: Developing a drop test set-up to characterize the performance of TNO’s HTP/ethanol hypergolic propellant combination

Long-life HTP depot refuelling interface: A preliminary investigation

Feasibility study of additive manufacturing techniques applicable to resistojet propulsion systems

In-orbit Refuelling with Hydrogen Peroxide: An Architecture and Transfer Mechanism

Thermal ignition system for green rocket propulsion: Experimental study on thermal ignition of high concentration hydrogen peroxide and ethanol propellant

Hydrocarbon Seeded ABS - Nitrous Hybrid Engine Development: Experimental Validation of an Analytical Design Tool

Highly concentrated H2O2 preparation, stabilization and decomposition over manganese oxide-based catalysts for space propulsion

Research and Development of a Combined Fuel Cell and Satellite Thruster System: Using Novel Hydrogen Peroxide Decomposition Techniques

Prototype X: A Cost-Based Design Optimization of an Upper Stage Liquid Propulsion Module with Green-Storable Propellants

Preliminary design of a rocket-based combined cycle engine for application aboard Mk-II Aurora suborbital spaceplane

A Novel Green Hybrid Hypergolic Bi-propellant with Viscoelastic Nature of the Fuel

Novel and Green Hypergolic Bi- Propellant System for Propulsion Application

The design and testing of an injector for anadvanced hypergolic dual-mode propulsionsystem

Transient Thermal Modelling of Cooling Methods in Green Bi-Propellant Thrusters for CubeSat Applications: A numerical and experimental comparison of regenerative cooling and radiation cooling in a CubeSat scale propulsion system

Design of a modular one Newton hydrogen peroxide monopropellant thruster, including feed system and test setup