PL430143A1 - Combustion chamber of a hybrid rocket engine - Google Patents

Combustion chamber of a hybrid rocket engine

Info

Publication number
PL430143A1
PL430143A1 PL430143A PL43014319A PL430143A1 PL 430143 A1 PL430143 A1 PL 430143A1 PL 430143 A PL430143 A PL 430143A PL 43014319 A PL43014319 A PL 43014319A PL 430143 A1 PL430143 A1 PL 430143A1
Authority
PL
Poland
Prior art keywords
fuel
combustion chamber
rocket engine
hybrid rocket
fuel pipe
Prior art date
Application number
PL430143A
Other languages
Polish (pl)
Other versions
PL242632B1 (en
Inventor
Robert Magiera
Adam Matusiewicz
Kacper Zieliński
Original Assignee
Spaceforest Spółka Z Ograniczoną Odpowiedzialnością
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Spaceforest Spółka Z Ograniczoną Odpowiedzialnością filed Critical Spaceforest Spółka Z Ograniczoną Odpowiedzialnością
Priority to PL430143A priority Critical patent/PL242632B1/en
Publication of PL430143A1 publication Critical patent/PL430143A1/en
Publication of PL242632B1 publication Critical patent/PL242632B1/en

Links

Abstract

Komora spalania hybrydowego silnika rakietowego mająca cylindryczną obudowę (1), wewnątrz której znajduje się ziarno paliwa i która z jednej strony zamknięta jest modułem wtryskowym (3), a z drugiej strony połączona jest z dyszą (2) charakteryzuje się tym, że ziarno paliwa składa się z połączonych ze sobą trwale: rury paliwowej (7) przylegającej szczelnie do obudowy (1), co najmniej jednego pręta paliwowego (8) znajdującego się w kanale rury paliwowej (7) i co najmniej jednego rusztu paliwowego (9) na końcu rury paliwowej (7).Combustion chamber of a hybrid rocket engine having a cylindrical housing (1) inside which there is a fuel grain and which on one side is closed with an injection module (3) and on the other side is connected to the nozzle (2), characterized in that the fuel grain consists of from permanently connected: a fuel pipe (7) tightly adjacent to the housing (1), at least one fuel rod (8) located in the channel of the fuel pipe (7) and at least one fuel grate (9) at the end of the fuel pipe ( 7).

PL430143A 2019-06-05 2019-06-05 Combustion chamber of a hybrid rocket engine PL242632B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL430143A PL242632B1 (en) 2019-06-05 2019-06-05 Combustion chamber of a hybrid rocket engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL430143A PL242632B1 (en) 2019-06-05 2019-06-05 Combustion chamber of a hybrid rocket engine

Publications (2)

Publication Number Publication Date
PL430143A1 true PL430143A1 (en) 2020-12-14
PL242632B1 PL242632B1 (en) 2023-03-27

Family

ID=73727680

Family Applications (1)

Application Number Title Priority Date Filing Date
PL430143A PL242632B1 (en) 2019-06-05 2019-06-05 Combustion chamber of a hybrid rocket engine

Country Status (1)

Country Link
PL (1) PL242632B1 (en)

Also Published As

Publication number Publication date
PL242632B1 (en) 2023-03-27

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