Lightweight, Cost-effective Composite and Green Bipropellant System for Space Transportation Applications

MSCA (Marie Skłodowska-Curie)HORIZON-TMA-MSCA-PF-EFID: 101107214
EC Contribution
€2,543
Consortium Size
2 orgs
Start Year
2023
Summary

Engineering novel materials and their design optimization using simulation-based tools enable the development of lightweight and sturdy thrusters. In Europe, the development of high-temperature-resistant structural materials for space transportation has gained momentum over the years. This has led to the increased usage of ceramic matrix composite over conventional metal alloys in aerospace applications. Most of the reported works focus on manufacturing cost-effective and lightweight composites, whereas the thermally stable nature of composites has not been fully explored. The Green Charter and European Green Deal promote low-emission forms of transport and emphasize developing sustainable and renewable forms of energy. The adoption of green fuels offers advantages in terms of total life cycle cost reduction, contributing to cheaper space transportation, and environmental impact reduction. Contemporary research innovations have expanded the development of ""green propellants"" for spacecraft in diverse space applications on a global level, primarily for eco-innovation and safety considerations. Studies with ammonium dinitramide, hydrazinium nitroformate with methanol, and ethanol-water are still in the nascent phase whereas H2O2 is delivering state-of-the-art performance to replace conventional hydrazine. This project aims to explore the possibility of developing a 1-100N class thruster made of thermally stable composite (carbon-ceramic) and green bipropellant (H2O2-Kerosene) system for the upper stage to reduce the overall weight, life cycle cost, and environmental impacts without compromising on the performance parameters. This will be researched through a comprehensive blend of multi-physics-based numerical modeling and analysis to generate a highly reliable design and a scale-specific experimental characterization and test rig to yield propellant formulation data corresponding to the state-of-the-art. The proposal will produce high societal, scientific, and economic impacts.""

Consortium (2)

Project Results (14)

Source: CORDIS, the EU research results database.

Publications (12)
Effect of Sintering Parameters on the Densification, Microstructure, and Mechanical Performance of ZrB <sub>2</sub> –SiC Ceramics
International Journal of Applied Ceramic Technology· 2026DOI
Prakhar Jindal, Iason Krinis, Vera Popovich, Hans Brouwer, Jyoti Botchu, Yinglu Tang
Experimental Investigation of Green Hypergolic Propellants for Upper-Stage Propulsion: Drop Test Results and Performance Analysis
IAF Space Propulsion Symposium· 2026DOI
Prakhar Jindal, Kyoungeun Lee, Jyoti Botchu Vara Siva
Kinetic and experimental study of Mn(III) acetylacetonate for green hypergolic ignition in HTP/Kerosene systems
Aerospace Science and Technology· 2026DOI
Prakhar Jindal, Jyoti Botchu
Kinetic and mechanistic analysis of Mn(II)AA doped hypergolic ignition in HTP/kerosene bipropellant systems
Results in Engineering· 2026DOI
Prakhar Jindal; Jyoti Botchu
Combustion and structural analysis of green bipropellant uhtcmc thrusters for upper-stage applications
· 2025
Prakhar Jindal, Tamim Doozandeh, Maximilian Pfohl, Jyoti Botchu Vara Siva
Ignition Delay Times of Conventional and Green Hypergolic Propellants at Ambient Conditions: A Comparative Review
Applied Sciences· 2025DOI
Prakhar Jindal, Jyoti Botchu Vara Siva
Kinetic and mechanistic analysis of Mn(II)AA doped hypergolic ignition in HTP/kerosene bipropellant systems
Results in Engineering· 2025DOI
Prakhar Jindal, Jyoti Botchu
Optimizing densification and mechanical properties of spark plasma sintered ZrB2-SiC ceramic composites
Ceramics International· 2025DOI
Krinis, Iason; Jindal, Prakhar; Popovich, Vera; Brouwer, Hans; Botchu, Jyoti; Tang, Yinglu
Optimizing densification and mechanical properties of spark plasma sintered ZrB2-SiC ceramic composites
Ceramics International· 2025DOI
Iason Krinis, Prakhar Jindal, Vera Popovich, Hans Brouwer, Jyoti Botchu, Yinglu Tang
Probabilistic Damage Modeling and Thermal Shock Risk Assessment of UHTCMC Thruster Under Transient Green Propulsion Operation
Materials· 2025DOI
Prakhar Jindal, Tamim Doozandeh, Jyoti Botchu
Sustainable Design and Wall Thickness Optimization for Enhanced Lifetime of Ultra-High Temperature Ceramic Matrix Composite Thruster for Use in Green Propulsion Systems
Materials· 2025DOI
Tamim Doozandeh, Prakhar Jindal, Jyoti Botchu
Performance Analysis of Injector Configurations in Green Unstaged Hypergolic Bipropellant Thrusters: A CFD Study Using Hydrogen Peroxide and Kerosene
· 2024
Maximilian Pfohl, Prakhar Jindal, Jyoti Botchu Vara Siva
Deliverables (1)
Data Management Plan
Other Results (1)
Periodic Reporting for period 1 - GREENLAM (Lightweight, Cost-effective Composite and Green Bipropellant System for Space Transportation Applications)