Expanded in 2023, the Chemical Research Laboratory for space applications enablesa  global-scale investigation of physico-chemical properties and chemical compatibility of propellant materials.

Łukasiewicz – Institute of Aviation is a leading research and development unit in Poland and worldwide in the field of ecological rocket propulsion. Its primary areas of interest and specialization lie in environmentally friendly liquid and hybrid propulsion systems based on over 98% hydrogen peroxide, as well as innovative hypergolic fuels.

The in-house capabilities of production of hydrogen peroxide with concentrations exceeding 98% are based on a patented method, providing independence in preparations for testing engines and other components utilizing HTP.

The chemical laboratory – tasks

• Research on fuels for new liquid, hybrid, and gel propulsion systems.
• Research onfuels hypergolic with hydrogen peroxide (production, long-term storage, passivation, and compatibility studies).
• Research on chemical durability of fuels containing catalytic and/or energetic additives.
• Investigation of physicochemical parameters useful for propulsion applications.
• Development of advanced low-smoke solid rocket propellant materials.
• Research on high-performance environmentally friendly fuels and oxidizers of a new generation.
• Development of catalysts for single-component propellant applications.
• Research on the chemical compatibility of different structural materials with working fluids.
• Development of fuel compositions that spontaneously react with hydrogen peroxide (hypergolic).

The chemical laboratory – equipment

• Nicolet iS50 FT-IR spectrometer with built-in ATR.
• Vhx 7000 digital microscope.
• laboratory muffle furnace type FCF 22 SHM.
• vibratory sieve shaker AS Control.
• planetary ball mill PM 100.
• stand for casting solid rocket propellant materials.

Prototypes of propellant materials obtained through casting process and after thermal conditioning must undergo testing to meet specified parameters, including ballistic, mechanical, thermochemical properties, and safety requirements. Only with a ready and properly characterized propellant material can full thruster tests be conducted, which are  performed on site on vacuum or atmospheric test stands. Consolidating the research facilities in one place enables comprehensive research and development of solid propellant materials while increasing their safety.