GB505747A - Improvements connected with rockets - Google Patents

Improvements connected with rockets

Info

Publication number
GB505747A
GB505747A GB718639A GB718639A GB505747A GB 505747 A GB505747 A GB 505747A GB 718639 A GB718639 A GB 718639A GB 718639 A GB718639 A GB 718639A GB 505747 A GB505747 A GB 505747A
Authority
GB
United Kingdom
Prior art keywords
propellent
nozzle
charge
propellent charge
rocket
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
GB718639A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB718639A priority Critical patent/GB505747A/en
Publication of GB505747A publication Critical patent/GB505747A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Inorganic Compounds Of Heavy Metals (AREA)

Abstract

505,747. Rockets. ZWER INA, R. Aug. 10, 1937, No, 7186/39. Divided application. [Classes 9 (i) and 9 (ii)] . A rocket is provided with a solid propellent charge which is so shaped that the combustion gases issuing therefrom are directed into the throat of the nozzle. In the construction shown, the charge comprisee separate layers t<1>, t<2> ... t<6>, the abutting surfaces of which are of spherical formation. The individual layers may be separated by, or wrapped in, suitable retarding material in order to control the rate of com-' bustion of the propellent charge during flight. The propellent charge is compacted by means of a cylindrical press having a hemispherical end, which is inserted into the nozzle end of the rocket casing a. The hemispherical end of the press may be provided with projections, which produce indentations in the surface of the propellent material nearest the nozzle b. The inner surface of the casing a may be conical, in order to aid the compacting of the propellent charge.
GB718639A 1937-08-10 1937-08-10 Improvements connected with rockets Expired GB505747A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB718639A GB505747A (en) 1937-08-10 1937-08-10 Improvements connected with rockets

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB718639A GB505747A (en) 1937-08-10 1937-08-10 Improvements connected with rockets

Publications (1)

Publication Number Publication Date
GB505747A true GB505747A (en) 1939-05-10

Family

ID=9828258

Family Applications (1)

Application Number Title Priority Date Filing Date
GB718639A Expired GB505747A (en) 1937-08-10 1937-08-10 Improvements connected with rockets

Country Status (1)

Country Link
GB (1) GB505747A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2422721A (en) * 1944-10-13 1947-06-24 William W Farr Rocket projectile
DE1167120B (en) * 1960-08-10 1964-04-02 Boelkow Entwicklungen Kg Solid rocket engine, the propellant body of which is designed as an internal star burner
US3266240A (en) * 1962-04-12 1966-08-16 Aerojet General Co Thrust control of solid propellant rockets
DE1241198B (en) * 1964-07-15 1967-05-24 Dynamit Nobel Ag Solid forehead burner propellant for rockets
US3811380A (en) * 1958-01-30 1974-05-21 Cava Ind Rocket and propellant therefor
US5537815A (en) * 1985-07-12 1996-07-23 Office National D'etudes Et De Recherches Aerospatiales Power units of the ram-jet engine type
CN114233517A (en) * 2021-12-21 2022-03-25 西安零壹空间科技有限公司 High-overload solid rocket engine and design method of explosive type thereof

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2422721A (en) * 1944-10-13 1947-06-24 William W Farr Rocket projectile
US3811380A (en) * 1958-01-30 1974-05-21 Cava Ind Rocket and propellant therefor
DE1167120B (en) * 1960-08-10 1964-04-02 Boelkow Entwicklungen Kg Solid rocket engine, the propellant body of which is designed as an internal star burner
US3266240A (en) * 1962-04-12 1966-08-16 Aerojet General Co Thrust control of solid propellant rockets
DE1241198B (en) * 1964-07-15 1967-05-24 Dynamit Nobel Ag Solid forehead burner propellant for rockets
US5537815A (en) * 1985-07-12 1996-07-23 Office National D'etudes Et De Recherches Aerospatiales Power units of the ram-jet engine type
CN114233517A (en) * 2021-12-21 2022-03-25 西安零壹空间科技有限公司 High-overload solid rocket engine and design method of explosive type thereof
CN114233517B (en) * 2021-12-21 2024-03-29 西安零壹空间科技有限公司 Solid rocket engine for high overload and drug pattern design method thereof

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