| Development of the ILR-33 “Amber” sounding rocket for microgravity experimentation B Marciniak, A Okninski, B Bartkowiak, M Pakosz, K Sobczak, W Florczuk, ... Aerospace Science and Technology 73, 19-31, 2018 | 48 | 2018 |
| Development of green storable hybrid rocket propulsion technology using 98% hydrogen peroxide as oxidizer A Okninski, P Surmacz, B Bartkowiak, T Mayer, K Sobczak, M Pakosz, ... Aerospace 8 (9), 234, 2021 | 33 | 2021 |
| The safe preparation of HTP and concentrated H2O2 samples G Rarata, P Surmacz Prace Instytutu Lotnictwa, 121-130, 2011 | 29 | 2011 |
| Aluminum Oxide–Supported Manganese Oxide Catalyst for a 98% Hydrogen Peroxide Thruster P Surmacz, M Kostecki, Z Gut, A Olszyna Journal of Propulsion and Power 35 (3), 614-623, 2019 | 26 | 2019 |
| Development of a small green bipropellant rocket engine using hydrogen peroxide as oxidizer A Okninski, B Bartkowiak, K Sobczak, D Kublik, P Surmacz, G Rarata, ... 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 3592, 2014 | 25 | 2014 |
| Hydrogen peroxide as a high energy compound optimal for propulsive applications G Rarata, K Rokicka, P Surmacz Central European Journal of Energetic Materials 13 (3), 778-790, 2016 | 24 | 2016 |
| Influence of various types of Al2O3/MnxOy catalysts on performance of a 100mm chamber for decomposition of 98%+ hydrogen peroxide P Surmacz Prace Instytutu Lotnictwa, 2015 | 23 | 2015 |
| Green rocket propulsion research and development at the institute of aviation: problems and perspectives P Surmacz Journal of KONES 23 (1), 337-344, 2016 | 17 | 2016 |
| Test campaign of a green liquid bi-propellant rocket engine using catalytically decomposed 98% hydrogen peroxide as oxidizer KM Sobczak, P Surmacz, B Bartkowiak, A Okninski, GP Rarata, ... 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 4926, 2017 | 13 | 2017 |
| Investigation of spontaneous ignition in a 100 N HTP/HTPB hybrid rocket engine P Surmacz, G Rarata Prace Instytutu Lotnictwa, 69--79, 2015 | 12 | 2015 |
| Near future green propellant for space transportation G Rarata, P Surmacz, K Sobczak VIII International Scientific Conference:“Development Trends in Space …, 2013 | 11 | 2013 |
| Hybrid rocket propulsion development and application P Surmacz, G Rarata Pr. Inst. Lotnictwa 3 (198), 123-137, 2009 | 9 | 2009 |
| Modern solid rocket propellants G Rarata, P Surmacz Prace Instytutu Lotnictwa 202, 112-124, 2009 | 9 | 2009 |
| Development Status of 500 N-class HTP/TMPDA Bi-propellant Rocket Engine P Surmacz, K Sobczak, B Bartkowiak, G Rarata, A Okninski, T Mayer, ... Proceedings of the 69th International Astronautical Congress, Bremen …, 2018 | 8 | 2018 |
| Experimental Evaluation of a Catalyst Bed Based on MnxOy/Al2O3 Catalyst for Decomposition of 98% Hydrogen Peroxide P Surmacz, GP Rarata, KM Sobczak, B Bartkowiak, A Okninski, ... 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 4923, 2017 | 8 | 2017 |
| Potential risk concerning the Use of Hydrogen Peroxide G Rarata, P Surmacz, W Florczuk AVT-210 Specialists Meeting on Risk and Reliability Assessment and …, 2013 | 8 | 2013 |
| Współczesne stałe rakietowe materiały pędne G Rarata, P Surmacz Prace Instytutu Lotnictwa, 112-124, 2009 | 8 | 2009 |
| Development of POLON—A Green Microsatellite Propulsion Module Utilizing 98% Hydrogen Peroxide J Gramatyka, P Paszkiewicz, D Grabowski, A Parzybut, D Bodych, ... Aerospace 9 (6), 297, 2022 | 7 | 2022 |
| Developing and testing new composite catalytic bed for decomposition of 98% HTP G Rarata, P Surmacz 65th International astronautical congress, toronto, 2014 | 7 | 2014 |
| Nadtlenek wodoru 98% klasy HTP-alternatywa dla hydrazyny G Rarata, P Surmacz Prace Instytutu Lotnictwa, 2014 | 6 | 2014 |
