GB1394401A - Solid-fuel rocket propulsion unit - Google Patents

Solid-fuel rocket propulsion unit

Info

Publication number
GB1394401A
GB1394401A GB159773A GB159773A GB1394401A GB 1394401 A GB1394401 A GB 1394401A GB 159773 A GB159773 A GB 159773A GB 159773 A GB159773 A GB 159773A GB 1394401 A GB1394401 A GB 1394401A
Authority
GB
United Kingdom
Prior art keywords
solid
air
envelope
propulsion unit
jan
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
GB159773A
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.)
Bayern Chemie Gesellschaft fuer Flugchemische Antriebe mbH
Original Assignee
Bayern Chemie Gesellschaft fuer Flugchemische Antriebe mbH
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
Priority claimed from DE19722204006 external-priority patent/DE2204006C3/en
Application filed by Bayern Chemie Gesellschaft fuer Flugchemische Antriebe mbH filed Critical Bayern Chemie Gesellschaft fuer Flugchemische Antriebe mbH
Publication of GB1394401A publication Critical patent/GB1394401A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/34—Casings; Combustion chambers; Liners thereof

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Laminated Bodies (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Thermal Insulation (AREA)

Abstract

1394401 Solid-fuel propulsion units BAYERN-CHEMIE GES FUR FLUGCHEMISCHE ANTRIEBE mbH 11 Jan 1973 [28 Jan 1972] 1597/73 Heading F3A A thermally insulated, solid-fuel propulsion unit for air-to-air missiles comprises a combustion chamber 4 separated from an outer envelope 1, to which stabilizing fins 18 are attached, by a gas-impermeable, annular gap 7 and thermal insulation 10, 11. The annular gap is either evacuated or filled with a gas of low thermal conductivity, e.g. air. The chamber 4 is formed of high-tensile steel and the envelope 1 is formed of titanium alloy or berylliumaluminium alloy. A threaded portion 16 of the envelope is provided for receiving a warhead. The insulation 10, 11 is formed of glass fibre impregnated with phenol resin.
GB159773A 1972-01-28 1973-01-11 Solid-fuel rocket propulsion unit Expired GB1394401A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19722204006 DE2204006C3 (en) 1972-01-28 Solid rocket engine, especially for missiles of the military type launched from high-speed aircraft

Publications (1)

Publication Number Publication Date
GB1394401A true GB1394401A (en) 1975-05-14

Family

ID=5834312

Family Applications (1)

Application Number Title Priority Date Filing Date
GB159773A Expired GB1394401A (en) 1972-01-28 1973-01-11 Solid-fuel rocket propulsion unit

Country Status (2)

Country Link
FR (1) FR2169067B3 (en)
GB (1) GB1394401A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2500149B1 (en) * 1981-02-17 1985-12-06 Poudres & Explosifs Ste Nale PROPULSIVE LOADING BIREGIME WITH TRUMPET HAVING A STAR SECTION

Also Published As

Publication number Publication date
FR2169067B3 (en) 1976-01-16
DE2204006B2 (en) 1975-10-09
DE2204006A1 (en) 1973-08-09
FR2169067A1 (en) 1973-09-07

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Legal Events

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