scholarly journals Postscript for Special Issue “Advances in Hybrid Rocket Technology and Related Analysis Methodologies”

Aerospace ◽  
2020 ◽  
Vol 7 (8) ◽  
pp. 117
Author(s):  
Carmine Carmicino
Keyword(s):  
Special Issue ◽  
Hybrid Rocket ◽  
Rocket Technology

Since the Editorial [...]

scholarly journals Special Issue “Advances in Hybrid Rocket Technology and Related Analysis Methodologies”

Aerospace ◽  
2019 ◽  
Vol 6 (12) ◽  
pp. 128 ◽  
Author(s):  
Carmine Carmicino
Keyword(s):  
Combustion Chamber ◽  
Solid Fuel ◽  
Special Issue ◽  
Hybrid Rocket ◽  
Propulsion Systems ◽  
Hybrid Rockets ◽  
Chemical Propulsion ◽  
Rocket Technology

Hybrid rockets are chemical propulsion systems that, in the most common configuration, employ a liquid oxidizer (or gaseous in much rarer cases) and a solid fuel; the oxidizer, stored in tanks, is properly injected in the combustion chamber where the solid fuel grain is bonded [...]

Sounding Rocket "HEROS" - A Low-Cost Hybrid Rocket Technology Demonstrator

2017 ◽  
Author(s):  
Mario Kobald ◽  
Ulrich Fischer ◽  
Konstantin Tomilin ◽  
Anna Petrarolo ◽  
Paula Kysela ◽  
...  
Keyword(s):  
Low Cost ◽  
Sounding Rocket ◽  
Hybrid Rocket ◽  
Rocket Technology ◽  
Technology Demonstrator

scholarly journals Development of Green Storable Hybrid Rocket Propulsion Technology Using 98% Hydrogen Peroxide as Oxidizer

Aerospace ◽  
2021 ◽  
Vol 8 (9) ◽  
pp. 234
Author(s):  
Adam Okninski ◽  
Pawel Surmacz ◽  
Bartosz Bartkowiak ◽  
Tobiasz Mayer ◽  
Kamil Sobczak ◽  
...  
Keyword(s):  
Hydrogen Peroxide ◽  
Research Network ◽  
Main Stage ◽  
Launch Vehicles ◽  
Hybrid Rocket ◽  
Space Propulsion ◽  
Sounding Rockets ◽  
Hybrid Propulsion ◽  
Rocket Propulsion ◽  
Rocket Technology

This paper presents the development of indigenous hybrid rocket technology, using 98% hydrogen peroxide as an oxidizer. Consecutive steps are presented, which started with interest in hydrogen peroxide and the development of technology to obtain High Test Peroxide, finally allowing concentrations of up to 99.99% to be obtained in-house. Hydrogen peroxide of 98% concentration (mass-wise) was selected as the workhorse for further space propulsion and space transportation developments. Over the course nearly 10 years of the technology’s evolution, the Lukasiewicz Research Network—Institute of Aviation completed hundreds of subscale hybrid rocket motor and component tests. In 2017, the Institute presented the first vehicle in the world to have demonstrated in-flight utilization for 98% hydrogen peroxide. This was achieved by the ILR-33 AMBER suborbital rocket, which utilizes a hybrid rocket propulsion as the main stage. Since then, three successful consecutive flights of the vehicle have been performed, and flights to the Von Karman Line are planned. The hybrid rocket technology developments are described. Advances in hybrid fuel technology are shown, including the testing of fuel grains. Theoretical studies and sizing of hybrid propulsion systems for spacecraft, sounding rockets and small launch vehicles have been performed, and planned further developments are discussed.

Integrated approach for hybrid rocket technology development

2016 ◽  
Vol 128 ◽  
pp. 257-261 ◽  
Author(s):  
Francesco Barato ◽  
Nicolas Bellomo ◽  
Daniele Pavarin
Keyword(s):  
Technology Development ◽  
Integrated Approach ◽  
Hybrid Rocket ◽  
Rocket Technology

Hybrid Rocket Technology

2011 ◽  
Vol 61 (3) ◽  
pp. 193-200 ◽  
Author(s):  
Sankaran Venugopal ◽  
K. Rajesh ◽  
V. Ramanujachari
Keyword(s):  
Hybrid Rocket ◽  
Rocket Technology
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