Technical Program

Technical Program

Technical Program

12th Development Trends in Space Propulsion Systems international conference

HYBRID EDITION 2021

27th October 2021
Venue: Łukasiewicz Research Network – Institute of Aviation
Building X, Main Conference Room
Krakowska 110/114, 02-256 Warsaw, Poland
09:00 – 10:00 Registration and welcome coffee
10:00 – 10:30

Conference opening:

Dr Sylwester Wyka
Deputy Director of Łukasiewicz Research Network – Institute of Aviation

Prof. Marek Moszyński
Vice-president of the Polish Space Agency

Gen. Mirosław Hermaszewski
Polish Cosmonaut

10:30 – 11:15 KEYNOTE PRESENTATION
Piotr Wolański, Adam Okniński: Development of Rocket Propulsion in Poland
SESSION 1: PROPULSION FOR SPACE TRANSPORTATION
i.e. Engines, Motors and Reaction Control Systems for Space Transportation
Chairman: Adam Okniński
11:15 – 11:30 Michał Kawalec First in-flight demonstration
of a rocket detonation engine using liquid propellants
Lukasiewicz Research Network
– Institute of Aviation
11:30 – 11:45 Bing Wang Rotating Detonation
and its Application as Rocket Engines
Tsinghua University
11:45 – 12:00 Tomasz Noga Testing of a 2 Newton cold-gas thruster developed for a Reaction Control System of a suborbital rocket Lukasiewicz Research Network
– Institute of Aviation
12:00 – 12:15 Adam Matusiewicz SF1000: hybrid rocket motor
in 1 MNs class – development
and testing
SpaceForest
12:15 – 12:30 Michał Pakosz The progress on the development of the ILR-33 AMBER 2K rocket Lukasiewicz Research Network – Institute of Aviation
12:30 – 12:45 COFFEE BREAK
SESSION 2: NUMERICAL MODELLING OF ROCKET PROPULSION SYSTEMS
i.e. Computational Fluid Dynamics, Heat Transfer Simulations, Internal Ballistics
Chairman: Krzysztof Benkiewicz
12:45 – 13:00 Andrej Sternin Trade-Off Analysis
of thermophysical models CFD-Simulations of CH4/O2 space engine combustion chambers
Technical University of Munich, Technical University of Dresden
13:00 – 13:15 Daniel Martínez-Sanchis Dynamic processes in thermal loads of rocket engines Technical University of Munich
13:15 – 13:30 Dawid Maleszyk Numerical study of heat transfer in resistojet rocket engine Warsaw University of Technology
13:30 – 13:45 Tiziano Santese Prediction of Thermo-Physical Properties of Commercially Available Methane Mixtures Technical University of Munich
13:45 – 14:00 Piotr Umiński Rocket Propulsion Analysis Tool Warsaw University of Technology
14:00 – 15:00 LUNCH & NETWORKING BREAK
SESSION 3: TESTING OF SPACE AND ROCKET PROPULSION SYSTEMS AND COMPONENTS
i.e. Rocket Engine and Thruster Hot-Firings, Component Testing, Instrumentation
Chairman: Andrej Sternin
15:00 – 15:15 Christian Krokstedt Testing of bi-liquid rocket engines for European Microlaunchers at Esrange Space Center Swedish Space Corporation
15:15 – 15:30 Tobiasz Mayer Lessons learned during development and usage of Propulsion Test Laboratory Lukasiewicz Research Network
– Institute of Aviation
15:30 – 15:45 Paweł Falek Practical consideration and advantages of piezoelectric based sensors for propulsion testing Kistler Instrumente
15:45 – 16:00 Krzysztof Bieńkowski Monostable 10 N Thruster Valve – lessons learned from the actuator level test campaign Astronika
16:00 – 16:15 Michał Sekrecki Cavitating venturi as a mass flow controller in deep throttling rocket engine Lukasiewicz Research Network – Institute of Aviation
16:15 – 16:30 COFFEE BREAK
SESSION 4: SPACECRAFT PROPULSION AND ADVANCED PROPULSION TECHNOLOGIES
i.e. Green Propulsion Systems, Propulsive Deorbit, Rotating Detonation Engines
Chairman: Jan Kindracki
16:30 – 16:45 Jakub Gramatyka An Overview & Current Development Status of the Polish Propulsion Module (POLON) Lukasiewicz Research Network
– Institute of Aviation
16:45 – 17:15 Hanna Tuchowska Development of Solid De-orbit Rocket Motor with dedicated Thrust Vector Control Lukasiewicz Research Network
– Institute of Aviation
17:15 – 17:30 Michał Kawalec Development of rocket engines utilizing rotating detonation At the Łukasiewicz – Institute of Aviation Lukasiewicz Research Network
– Institute of Aviation
17:45 – 18:00 Andrzej Kotarski Iterative design process in optimization of High Power Rocket Polish Astronautical Society
18:00 – 18:15 CONCLUDING REMARKS AND CONFERENCE CLOSURE
Piotr Wolański
18:15 – 19:30 FAREWELL RECEPTION

ADDITIONAL POSTER EXHIBITION to be found in the coffeebreak area: Magnetron cylindrical plasma sources
(Dr Marek Betiuk, Mr. Piotr Domanowski from Łukasiewicz Research Network – Institute of Precision Mechanics)

ADDITIONAL POSTER EXHIBITION to be found in the coffeebreak area: Magnetron cylindrical plasma sources
(Dr Marek Betiuk, Mr. Piotr Domanowski from Łukasiewicz Research Network – Institute of Precision Mechanics)

The Technical Program is based upon academic papers selected through the paper submission and review process.

In this matter, the Technical Program Committee is responsible for ensuring a well-balanced, high-quality conference program. The committee handles all issues related to paper submission, review and selection and the establishment of the final conference program.

Conference topics:

  • Space propulsion systems (includes solid, liquid and hybrid rocket engines and motors, space electric propulsion, component and system level)
  • Green propellants (includes development, handling, testing and utilisation of environmentally friendly propellants)
  • Suborbital vehicles and payloads (suborbital demontrators, vehicles, microgravity research, atmosphere sounding)
  • Launch vehicles (launcher components and systems development and utilisation, micro-launchers concepts)
  • Rocket, launcher and spacecraft avionics (rocket and spacecraft TT&C systems, power systems, GNC, on-board computers)
  • Numerical modeling (rocket and spacecraft dynamics, aerothermodynamics, numerical tools)
  • Small satellites (small satellites platforms, subsystems and components, constellations)
  • AIV and test facilities (rocket engines and motors test stands, assembly, integration and verification infrastructure for rockets and spacecraft, test ranges)
  • Other related topics (other topics related to space propulsion design, development or applications)

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