ES314075A1 - Improvements improved in the stabilized combustión propulsion load bodies. (Machine-translation by Google Translate, not legally binding) - Google Patents

Improvements improved in the stabilized combustión propulsion load bodies. (Machine-translation by Google Translate, not legally binding)

Info

Publication number
ES314075A1
ES314075A1 ES0314075A ES314075A ES314075A1 ES 314075 A1 ES314075 A1 ES 314075A1 ES 0314075 A ES0314075 A ES 0314075A ES 314075 A ES314075 A ES 314075A ES 314075 A1 ES314075 A1 ES 314075A1
Authority
ES
Spain
Prior art keywords
translation
machine
stabilized
legally binding
*** translate
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
ES0314075A
Other languages
Spanish (es)
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.)
Nitrochemie Aschau GmbH
Original Assignee
Nitrochemie Aschau GmbH
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 Nitrochemie Aschau GmbH filed Critical Nitrochemie Aschau GmbH
Publication of ES314075A1 publication Critical patent/ES314075A1/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
    • 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
    • F02K9/18—Shape or structure of solid propellant charges of the internal-burning type having a star or like shaped internal cavity

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Cosmetics (AREA)
  • Acyclic And Carbocyclic Compounds In Medicinal Compositions (AREA)

Abstract

Improvements introduced in the stabilized combustion propulsion load bodies, characterized in that they are crossed through or through to a determined depth of their combustion surface with grooves or grooves in the form of a slot again filled with an appropriate material. (Machine-translation by Google Translate, not legally binding)
ES0314075A 1964-09-02 1965-06-11 Improvements improved in the stabilized combustión propulsion load bodies. (Machine-translation by Google Translate, not legally binding) Expired ES314075A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEN25457A DE1224097B (en) 1964-09-02 1964-09-02 Rocket propellant

Publications (1)

Publication Number Publication Date
ES314075A1 true ES314075A1 (en) 1966-03-01

Family

ID=7343440

Family Applications (1)

Application Number Title Priority Date Filing Date
ES0314075A Expired ES314075A1 (en) 1964-09-02 1965-06-11 Improvements improved in the stabilized combustión propulsion load bodies. (Machine-translation by Google Translate, not legally binding)

Country Status (8)

Country Link
BE (1) BE668813A (en)
CH (1) CH433869A (en)
DE (1) DE1224097B (en)
ES (1) ES314075A1 (en)
FR (1) FR1445331A (en)
GB (1) GB1126068A (en)
NL (1) NL6506300A (en)
SE (1) SE318747B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2500149B1 (en) * 1981-02-17 1985-12-06 Poudres & Explosifs Ste Nale PROPULSIVE LOADING BIREGIME WITH TRUMPET HAVING A STAR SECTION
EP0315618A1 (en) * 1987-11-04 1989-05-10 NORICUM MASCHINENBAU UND HANDEL GESELLSCHAFT m.b.H. Solid propellant charge

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3050435A (en) * 1957-10-24 1962-08-21 Phillips Petroleum Co Method of consolidating solid rocket propellant grains
US3054353A (en) * 1958-09-23 1962-09-18 Norman L Rumpp Segment grain
US3064423A (en) * 1959-04-22 1962-11-20 Hercules Powder Co Ltd Gas-generating device

Also Published As

Publication number Publication date
SE318747B (en) 1969-12-15
FR1445331A (en) 1966-07-08
DE1224097B (en) 1966-09-01
CH433869A (en) 1967-04-15
NL6506300A (en) 1966-03-03
BE668813A (en) 1966-02-28
GB1126068A (en) 1968-09-05

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