DE2219981A1 - Anordnung und Einrichtung in einem Flugzeug für Heißdampfbetrieb - Google Patents

Anordnung und Einrichtung in einem Flugzeug für Heißdampfbetrieb

Info

Publication number
DE2219981A1
DE2219981A1 DE19722219981 DE2219981A DE2219981A1 DE 2219981 A1 DE2219981 A1 DE 2219981A1 DE 19722219981 DE19722219981 DE 19722219981 DE 2219981 A DE2219981 A DE 2219981A DE 2219981 A1 DE2219981 A1 DE 2219981A1
Authority
DE
Germany
Prior art keywords
aircraft according
supply
combustion chamber
nozzle
aircraft
Prior art date
Legal status (The legal status 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 status listed.)
Pending
Application number
DE19722219981
Other languages
German (de)
English (en)
Inventor
Richard Ing. Wien Bargmann
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
WENDLING G
Original Assignee
WENDLING G
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 WENDLING G filed Critical WENDLING G
Publication of DE2219981A1 publication Critical patent/DE2219981A1/de
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44Feeding propellants
    • F02K9/52Injectors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60Constructional parts; Details not otherwise provided for
    • F02K9/62Combustion or thrust chambers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/72Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid and solid propellants, i.e. hybrid rocket-engine plants
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/97Rocket nozzles
    • F02K9/974Nozzle- linings; Ablative coatings

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
DE19722219981 1971-04-23 1972-04-24 Anordnung und Einrichtung in einem Flugzeug für Heißdampfbetrieb Pending DE2219981A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
AT355071A AT313713B (de) 1971-04-23 1971-04-23 Flugzeug

Publications (1)

Publication Number Publication Date
DE2219981A1 true DE2219981A1 (de) 1972-11-30

Family

ID=3552056

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19722219981 Pending DE2219981A1 (de) 1971-04-23 1972-04-24 Anordnung und Einrichtung in einem Flugzeug für Heißdampfbetrieb

Country Status (3)

Country Link
AT (1) AT313713B (no)
CH (1) CH562399A5 (no)
DE (1) DE2219981A1 (no)

Also Published As

Publication number Publication date
AT313713B (de) 1974-02-25
CH562399A5 (no) 1975-05-30

Similar Documents

Publication Publication Date Title
DE2842032A1 (de) Verfahren und vorrichtung zum verbrennen kohlenstoffhaltiger brennstoffe
DE4028224A1 (de) Waffe
DE202017006759U1 (de) Vorrichtung und System zur Steuerung von Flugkörpern und Kill-Vehicles, die mit gelförmigen Treibstoffen betrieben wird
DE2219981A1 (de) Anordnung und Einrichtung in einem Flugzeug für Heißdampfbetrieb
DE2723517C3 (de) Zündvorrichtung für einen Block brennbaren Pulvers
EP0078893B1 (de) Gesteuertes Geschoss
DE1064760B (de) Zuendeinrichtung fuer Brennkammern von Rueckstossantrieben
DE60216671T2 (de) Anzünder für Treibladungen
WO1987003355A1 (en) Process for raising the temperature of catalysts and device for performing the process
DE1626101B1 (de) Treibstoffversorgungssystem für ein Raketentriebwerk
DE19924907B4 (de) Feststofftriebwerk für eine Staustrahlrakete
DE3226269A1 (de) Teilverbrennbarer treibladungsanzuender
DE4130377A1 (de) Brenner fuer dieselmotorenabgas-partikelfilter
DE102008029150A1 (de) Gasgenerator
DE194853C (no)
DE2623582C2 (de) Raketengeschoß mit Ausklappleitwerk und Treibspiegel
DE113747C (no)
DE3204477C1 (de) Flugkörper mit Hilfsflüssigkeitssystem
EP0189545A1 (de) Luftatmender Feststoff-Staustrahlantrieb
DE1626101C (de) Treibstoffversorgungssystem fur ein Raketentriebwerk
EP4211343A1 (de) Schubkammervorrichtung und verfahren zum betreiben einer schubkammervorrichtung
DE1199659B (de) Treibladungskartusche fuer Feuerwaffen aller Art
CH454538A (de) Abgasverbrenner
DE1950407C (de) Treibstoffversorgungssystem für ein Raketentriebwerk
DE347854C (de) Gasturbine mit pendelnder Fluessigkeit als Treibmittel