GB941620A - Steering device for rocket powered vehicles - Google Patents

Steering device for rocket powered vehicles

Info

Publication number
GB941620A
GB941620A GB4035060A GB4035060A GB941620A GB 941620 A GB941620 A GB 941620A GB 4035060 A GB4035060 A GB 4035060A GB 4035060 A GB4035060 A GB 4035060A GB 941620 A GB941620 A GB 941620A
Authority
GB
United Kingdom
Prior art keywords
steering device
nozzle
powered vehicles
rocket powered
plastic
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
GB4035060A
Inventor
Harold W Ritchey
Allan Eugene Williams
Charles Spurgeon Roberts Jr
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
Priority to GB4035060A priority Critical patent/GB941620A/en
Publication of GB941620A publication Critical patent/GB941620A/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
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/84—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using movable nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)

Abstract

941,620. Controlling rockets. THIOKOL CHEMICAL CORPORATION. Nov. 23, 1960, No. 40350/60. Heading B7G. [Also in Division F3] The rocket motor casing 10 is coupled to the discharge nozzle 36 by the tubular bellows 38 and tilting of the nozzle relatively to the casing longitudinal axis is effected by the hydraulic cylinder 28. The solid propellant 14 is bonded to 10 by the plastic liner 12. The direct incidence of combustion gases on 38 is prevented by the plastic extension 40 and baffle 42. The nozzle throat is defined by the graphite insert 44.
GB4035060A 1960-11-23 1960-11-23 Steering device for rocket powered vehicles Expired GB941620A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB4035060A GB941620A (en) 1960-11-23 1960-11-23 Steering device for rocket powered vehicles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4035060A GB941620A (en) 1960-11-23 1960-11-23 Steering device for rocket powered vehicles

Publications (1)

Publication Number Publication Date
GB941620A true GB941620A (en) 1963-11-13

Family

ID=10414443

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4035060A Expired GB941620A (en) 1960-11-23 1960-11-23 Steering device for rocket powered vehicles

Country Status (1)

Country Link
GB (1) GB941620A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112211749A (en) * 2020-09-18 2021-01-12 西北工业大学 Small solid rocket engine
CN113339157A (en) * 2021-06-16 2021-09-03 西安交通大学 Variable thrust's miniature solid rocket engine flexible nozzle system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112211749A (en) * 2020-09-18 2021-01-12 西北工业大学 Small solid rocket engine
CN113339157A (en) * 2021-06-16 2021-09-03 西安交通大学 Variable thrust's miniature solid rocket engine flexible nozzle system

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