GB1038562A - Rocket motor and method of construction - Google Patents

Rocket motor and method of construction

Info

Publication number
GB1038562A
GB1038562A GB1858963A GB1858963A GB1038562A GB 1038562 A GB1038562 A GB 1038562A GB 1858963 A GB1858963 A GB 1858963A GB 1858963 A GB1858963 A GB 1858963A GB 1038562 A GB1038562 A GB 1038562A
Authority
GB
United Kingdom
Prior art keywords
grain
head plate
exhaust nozzle
moulded
secured
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
GB1858963A
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 GB1038562A publication Critical patent/GB1038562A/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
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/34—Casings; Combustion chambers; Liners thereof

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Adhesives Or Adhesive Processes (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

1,038,562. Rocket motors. THIOKOL CHEMICAL CORPORATION. May 10, 1963 [May 10, 1962], No. 18589/63. Heading F3A. A rocket motor comprises a moulded solid propellant grain having a head plate and exhaust nozzle secured thereto and a motor casing consisting of a filamentary material wound around the grain and overlapping the peripheral ends of the head plate and exhaust nozzle. A precast solid propellant grain 11 is fused at one end to a curved head plate 12 and an exhaust nozzle 14 at the other end. A filament tape 22 of glass, plastics or metallic wire with an epoxide bonding agent is wound on to the grain in successive layers and extends over the peripheral edges of the head plate 12 and nozzle 14 to retain these in place. The bonding agent is then cured so that the casing and grain become an integral structure. The grain is moulded with a tapered star-shaped axial cavity 17 and to facilitate winding the tape a mandrel 18 may be secured in the cavity and mounted for rotation in a lathe. As well as circular windings being applied as shown in Fig. 1, longitudinal windings are described which provide better retention of the end pieces. Other bonding agents are phenolics, polyesters and silicones.
GB1858963A 1962-05-10 1963-05-10 Rocket motor and method of construction Expired GB1038562A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US19383362A 1962-05-10 1962-05-10

Publications (1)

Publication Number Publication Date
GB1038562A true GB1038562A (en) 1966-08-10

Family

ID=22715201

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1858963A Expired GB1038562A (en) 1962-05-10 1963-05-10 Rocket motor and method of construction

Country Status (5)

Country Link
BE (1) BE632158A (en)
CH (1) CH414264A (en)
DE (1) DE1944134U (en)
GB (1) GB1038562A (en)
NL (2) NL292576A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2123036A1 (en) * 1969-11-24 1972-09-08 Nord Aviat
RU2505696C1 (en) * 2012-11-01 2014-01-27 Открытое акционерное общество Центральный научно-исследовательский институт специального машиностроения Method of making rocket engine housing from polymer composites and rocket engine housing from polymer composites
RU2566206C1 (en) * 2014-06-23 2015-10-20 Общество с ограниченной ответственностью "Базальт-Инвест" Production of rocket engine body
CN113958424A (en) * 2021-08-20 2022-01-21 西安零壹空间科技有限公司 Rocket boosting engine with inner trajectory curve free of tail warping phenomenon

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2402853A1 (en) * 1977-09-09 1979-04-06 Serat WEAPON SYSTEM, ESPECIALLY INFANTRY ANTICHAR
CN111810318B (en) * 2020-06-28 2022-04-22 北京凌空天行科技有限责任公司 Single-chamber double-thrust solid rocket engine and rocket

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2123036A1 (en) * 1969-11-24 1972-09-08 Nord Aviat
RU2505696C1 (en) * 2012-11-01 2014-01-27 Открытое акционерное общество Центральный научно-исследовательский институт специального машиностроения Method of making rocket engine housing from polymer composites and rocket engine housing from polymer composites
RU2566206C1 (en) * 2014-06-23 2015-10-20 Общество с ограниченной ответственностью "Базальт-Инвест" Production of rocket engine body
CN113958424A (en) * 2021-08-20 2022-01-21 西安零壹空间科技有限公司 Rocket boosting engine with inner trajectory curve free of tail warping phenomenon
CN113958424B (en) * 2021-08-20 2022-12-06 西安零壹空间科技有限公司 Rocket boosting engine with inner trajectory curve free of tail warping phenomenon

Also Published As

Publication number Publication date
BE632158A (en)
CH414264A (en) 1966-05-31
NL292576A (en)
NL131874C (en)
DE1944134U (en) 1966-08-11

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