GB1313898A - Method of reducing the disturbance behind and exhaust nozzle of a rocket propulsion unit - Google Patents

Method of reducing the disturbance behind and exhaust nozzle of a rocket propulsion unit

Info

Publication number
GB1313898A
GB1313898A GB3318870A GB3318870A GB1313898A GB 1313898 A GB1313898 A GB 1313898A GB 3318870 A GB3318870 A GB 3318870A GB 3318870 A GB3318870 A GB 3318870A GB 1313898 A GB1313898 A GB 1313898A
Authority
GB
United Kingdom
Prior art keywords
propulsion unit
exhaust nozzle
rocket propulsion
reducing
propellant
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.)
Expired
Application number
GB3318870A
Other languages
English (en)
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Publication of GB1313898A publication Critical patent/GB1313898A/en
Expired legal-status Critical Current

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06D—MEANS FOR GENERATING SMOKE OR MIST; GAS-ATTACK COMPOSITIONS; GENERATION OF GAS FOR BLASTING OR PROPULSION (CHEMICAL PART)
    • C06D3/00—Generation of smoke or mist (chemical part)
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Botany (AREA)
  • Pest Control & Pesticides (AREA)
  • Plant Pathology (AREA)
  • Organic Chemistry (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles (AREA)
  • Testing Of Engines (AREA)
GB3318870A 1969-07-09 1970-07-08 Method of reducing the disturbance behind and exhaust nozzle of a rocket propulsion unit Expired GB1313898A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR6923403A FR2052048A5 (enExample) 1969-07-09 1969-07-09

Publications (1)

Publication Number Publication Date
GB1313898A true GB1313898A (en) 1973-04-18

Family

ID=9037224

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3318870A Expired GB1313898A (en) 1969-07-09 1970-07-08 Method of reducing the disturbance behind and exhaust nozzle of a rocket propulsion unit

Country Status (2)

Country Link
FR (1) FR2052048A5 (enExample)
GB (1) GB1313898A (enExample)

Also Published As

Publication number Publication date
DE2034187A1 (de) 1971-01-21
FR2052048A5 (enExample) 1971-04-09

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee