GB1135541A - Improvements in rockets - Google Patents

Improvements in rockets

Info

Publication number
GB1135541A
GB1135541A GB1449665A GB1449665A GB1135541A GB 1135541 A GB1135541 A GB 1135541A GB 1449665 A GB1449665 A GB 1449665A GB 1449665 A GB1449665 A GB 1449665A GB 1135541 A GB1135541 A GB 1135541A
Authority
GB
United Kingdom
Prior art keywords
rocket
motor
auxiliary
casing
explosive charge
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
GB1449665A
Inventor
William Conrad Steph Schermuly
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.)
Schermuly Ltd
Original Assignee
Schermuly Ltd
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 Schermuly Ltd filed Critical Schermuly Ltd
Priority to GB1449665A priority Critical patent/GB1135541A/en
Publication of GB1135541A publication Critical patent/GB1135541A/en
Expired 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
    • F02K9/74Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant
    • F02K9/76Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with another rocket-engine plant; Multistage rocket-engine plants
    • F02K9/763Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with another rocket-engine plant; Multistage rocket-engine plants with solid propellant

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

1,135,541. Rockets. SCHERMULY Ltd. 5 April, 1966 [6 April, 1965], No. 14496/65. Heading F3A. A solid fuel rocket, particularly for use as a signalling device, anti-radar, anti-hail, or rain-making device having a maximum altitude of 10,000 feet comprises a main casing 1, e.g. of aluminium, housing a rocket motor 6, a detachably secured auxiliary casing 13 housing a rocket motor 18, and an explosive charge 21 situated between the two motors, the explosive charge 21 being ignitable by the burning of the rocket motor in the auxiliary casing and serving to both ignite the motor in the main casing and to separate the auxiliary casing from the main casing. The explosive charge 21 extends into a recess 23 in the motor 18 so that it explodes before the rocket motor 18 is completely burnt out. The rocket may comprise a number of auxiliary casings and motors each ignitable and separable by an interposed explosive charge. A payload 8 such as an illuminating signal, a parachute flare or an anti-radar device is ejected from the rocket on ignition of a charge 9. The main and auxiliary casings are provided with skirts 3 and 15 each having apertures 12 and serving as stabilizing tails in flight.
GB1449665A 1965-04-06 1965-04-06 Improvements in rockets Expired GB1135541A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1449665A GB1135541A (en) 1965-04-06 1965-04-06 Improvements in rockets

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1449665A GB1135541A (en) 1965-04-06 1965-04-06 Improvements in rockets

Publications (1)

Publication Number Publication Date
GB1135541A true GB1135541A (en) 1968-12-04

Family

ID=10042237

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1449665A Expired GB1135541A (en) 1965-04-06 1965-04-06 Improvements in rockets

Country Status (1)

Country Link
GB (1) GB1135541A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0354692A1 (en) * 1988-08-03 1990-02-14 Thiokol Corporation Case for a multiple or staged solid propellant rocket motor
GB2244795A (en) * 1978-10-19 1991-12-11 Rheinmetall Gmbh Armour piercing projectiles
US5431106A (en) * 1985-06-05 1995-07-11 Shorts Missile Systems Limited Release of daughter missiles

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2244795A (en) * 1978-10-19 1991-12-11 Rheinmetall Gmbh Armour piercing projectiles
GB2244795B (en) * 1978-10-19 1992-09-09 Rheinmetall Gmbh Penetrator for armour
US5431106A (en) * 1985-06-05 1995-07-11 Shorts Missile Systems Limited Release of daughter missiles
EP0354692A1 (en) * 1988-08-03 1990-02-14 Thiokol Corporation Case for a multiple or staged solid propellant rocket motor

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