GB1011007A - Rocket motor ignition system - Google Patents

Rocket motor ignition system

Info

Publication number
GB1011007A
GB1011007A GB3730763A GB3730763A GB1011007A GB 1011007 A GB1011007 A GB 1011007A GB 3730763 A GB3730763 A GB 3730763A GB 3730763 A GB3730763 A GB 3730763A GB 1011007 A GB1011007 A GB 1011007A
Authority
GB
United Kingdom
Prior art keywords
motors
rocket
reservoir
high temperature
solid 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
GB3730763A
Other languages
English (en)
Inventor
Richard Pursley King
James Robert Thurston
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.)
ATK Launch Systems LLC
Original Assignee
Thiokol Corp
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 Thiokol Corp filed Critical Thiokol Corp
Publication of GB1011007A publication Critical patent/GB1011007A/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
    • F02K9/95Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by starting or ignition means or arrangements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers
    • F41F3/04Rocket or torpedo launchers for rockets

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Air Bags (AREA)
GB3730763A 1963-11-06 1963-09-23 Rocket motor ignition system Expired GB1011007A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH1361863A CH423362A (de) 1963-11-06 1963-11-06 Zündvorrichtung zum gleichzeitigen Zünden einer Mehrzahl von Raketenmotoren eines Raketentriebwerkes

Publications (1)

Publication Number Publication Date
GB1011007A true GB1011007A (en) 1965-11-24

Family

ID=4393933

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3730763A Expired GB1011007A (en) 1963-11-06 1963-09-23 Rocket motor ignition system

Country Status (4)

Country Link
BE (1) BE637817A (nl)
CH (1) CH423362A (nl)
GB (1) GB1011007A (nl)
NL (1) NL298754A (nl)

Also Published As

Publication number Publication date
CH423362A (de) 1966-10-31
BE637817A (nl)
NL298754A (nl)

Similar Documents

Publication Publication Date Title
GB1102625A (en) Stabilisation and guidance device for sounding rockets and rocket-propelled ballistic vehicles
GB1051972A (nl)
US2935846A (en) Reaction motor feed system
US3115008A (en) Integral rocket ramjet missile propulsion system
GB1216200A (en) Multi-stage solid fuel rocket
US3336753A (en) Propulsion devices
GB1011007A (en) Rocket motor ignition system
US3230701A (en) Two step reaction propulsion method
US3217489A (en) Rocket motor ignition system
US3070014A (en) Jet propulsion device
US3518828A (en) Hybrid rocket motor ignition system
US3107487A (en) Rocket motor
US3345822A (en) Burning rate control of solid propellants
GB1120391A (en) Improvements in or relating to rocketwise propelled projectiles
GB1245707A (en) Solid propellant rocket engine
GB1473749A (en) Monopropellant thruster with superheater
GB961001A (en) Improvements in propulsion units having a plurality of reaction propulsion nozzles
GB844245A (en) Improvements in or relating to rocket motors
US3254603A (en) Hypergolic igniter
GB1164656A (en) Rocket Engines
GB1118078A (en) Composite ramjet/rocket propulsion unit
US11846252B2 (en) Propulsion system with initiators for selective activation of multiple rocket motors
GB1292279A (en) Improvements in or relating to thrust-vector-control systems
SORKIN Gas dynamics and thermodynamics of solid- propellant rockets(Soviet book on gas thermodynamics of solid propellant rocket engines covering combustion products equilibrium in nozzle and chamber, engine design, etc)
ISAACSON et al. Effect of chamber pressure on the burning rate of a composite, double-base, solid propellant rocket motor