GB1109284A - Improvements in or relating to frontal burner propellent charges for rockets - Google Patents

Improvements in or relating to frontal burner propellent charges for rockets

Info

Publication number
GB1109284A
GB1109284A GB2996465A GB2996465A GB1109284A GB 1109284 A GB1109284 A GB 1109284A GB 2996465 A GB2996465 A GB 2996465A GB 2996465 A GB2996465 A GB 2996465A GB 1109284 A GB1109284 A GB 1109284A
Authority
GB
United Kingdom
Prior art keywords
block
rockets
ignited
propellant
frontal
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
GB2996465A
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.)
Dynamit Nobel AG
Original Assignee
Dynamit Nobel AG
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 Dynamit Nobel AG filed Critical Dynamit Nobel AG
Publication of GB1109284A publication Critical patent/GB1109284A/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
    • F02K9/10—Shape or structure of solid propellant charges
    • F02K9/12—Shape or structure of solid propellant charges made of two or more portions burning at different rates or having different characteristics

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Evaporation-Type Combustion Burners (AREA)
  • Thermotherapy And Cooling Therapy Devices (AREA)

Abstract

1,109,284. Propellant charges for rockets. DYNAMIT NOBEL A.G. 14 July, 1965 [15 July, 1964], No. 29964/65. Heading F3A. A two-stage rocket propellant charge intended to be ignited at the forward end comprises a block 1 of quick-burning propellant and a block 2 of slower burning propellant. The block 1 when ignited at its forward end 7 produces the launching thrust and block 2 maintains the cruising velocity of the rocket. The abutting surfaces of the two blocks have a different area from the ignition surface 7 and are preferably spherical so that part of block is ignited before block 1 has burnt out. Insulation 8 covers the outer surfaces of the two blocks and they are separated by an impervious foil 6.
GB2996465A 1964-07-15 1965-07-14 Improvements in or relating to frontal burner propellent charges for rockets Expired GB1109284A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE1964D0044947 DE1241198B (en) 1964-07-15 1964-07-15 Solid forehead burner propellant for rockets

Publications (1)

Publication Number Publication Date
GB1109284A true GB1109284A (en) 1968-04-10

Family

ID=7048668

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2996465A Expired GB1109284A (en) 1964-07-15 1965-07-14 Improvements in or relating to frontal burner propellent charges for rockets

Country Status (6)

Country Link
BE (1) BE666866A (en)
DE (1) DE1241198B (en)
FR (1) FR1435429A (en)
GB (1) GB1109284A (en)
IL (1) IL23864A (en)
NL (1) NL6509162A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3210536A1 (en) * 1982-03-23 1983-09-29 Bayern-Chemie Gesellschaft für flugchemische Antriebe mbH, 8261 Aschau COMPOSITE DRIVE KIT AND METHOD FOR THE PRODUCTION THEREOF

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB505747A (en) * 1937-08-10 1939-05-10 Rudolf Zwerina Improvements connected with rockets
US2600678A (en) * 1949-03-11 1952-06-17 Olin Ind Inc Rocket powder

Also Published As

Publication number Publication date
NL6509162A (en) 1966-01-17
BE666866A (en) 1965-11-03
FR1435429A (en) 1966-04-15
IL23864A (en) 1969-04-30
DE1241198B (en) 1967-05-24

Similar Documents

Publication Publication Date Title
GB1428412A (en) Solid fuel rocket motors
GB1469665A (en) Warhead
GB1510986A (en) Projectile with an ejectable payload
GB1229119A (en)
GB1216200A (en) Multi-stage solid fuel rocket
GB1171705A (en) Improvements in or relating to Solid Fuel Rocket Propulsion Units
US2814179A (en) Return burning motor
GB1169079A (en) Practice Ammunition
GB1465550A (en) Projectile launching device
GB1470906A (en) Safety devices for projectiles
GB1317462A (en) Switch elements for mechanical actuation
GB1430750A (en) Fragmentation warhead for use in missiles
GB1109284A (en) Improvements in or relating to frontal burner propellent charges for rockets
US3029734A (en) Separation of stages in a staged rocket
GB1321588A (en) Spinstabilised rocket-propelled projectile
GB1015375A (en) Propellent charge for solid fuel rockets
FR2385075A1 (en) Charge scattering rocket propulsion system - has igniter charge to actuate excess of propulsive charge to destroy remaining parts
GB1120391A (en) Improvements in or relating to rocketwise propelled projectiles
USH203H (en) Integral rocket motor-warhead
GB1245707A (en) Solid propellant rocket engine
GB1074307A (en) Surface igniter for combustible charges
GB1361245A (en) Finstabilised projectiles
SE8804426L (en) SETTING AND DEVICE TO ACHIEVE INITIATION AND EXTRA FAST OVERTURNING OF POWDER AND PYROTECHNICAL KITS OF OPERETREED THE TYPE THAT IS LARGE LONG IN THE CREATIVE SECTION TO ITS SECTION
GB1320158A (en) Spring urged pyrotechnically actuated control elements
GB1242227A (en) Missiles comprising a rocket motor and a warhead-arming delay device