FR2299520A1 - Dispositif de decoupe d'elements structuraux d'un propulseur - Google Patents

Dispositif de decoupe d'elements structuraux d'un propulseur

Info

Publication number
FR2299520A1
FR2299520A1 FR7503339A FR7503339A FR2299520A1 FR 2299520 A1 FR2299520 A1 FR 2299520A1 FR 7503339 A FR7503339 A FR 7503339A FR 7503339 A FR7503339 A FR 7503339A FR 2299520 A1 FR2299520 A1 FR 2299520A1
Authority
FR
France
Prior art keywords
rocket
braking
blown out
explosive charge
explosion
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.)
Withdrawn
Application number
FR7503339A
Other languages
English (en)
Inventor
Luscan
Lacoste
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.)
Societe Europeenne de Propulsion SEP SA
Original Assignee
Societe Europeenne de Propulsion SEP SA
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 Societe Europeenne de Propulsion SEP SA filed Critical Societe Europeenne de Propulsion SEP SA
Priority to FR7503339A priority Critical patent/FR2299520A1/fr
Publication of FR2299520A1 publication Critical patent/FR2299520A1/fr
Withdrawn legal-status Critical Current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
    • F02K9/80Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/92Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control incorporating means for reversing or terminating thrust
FR7503339A 1975-01-29 1975-01-29 Dispositif de decoupe d'elements structuraux d'un propulseur Withdrawn FR2299520A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7503339A FR2299520A1 (fr) 1975-01-29 1975-01-29 Dispositif de decoupe d'elements structuraux d'un propulseur

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7503339A FR2299520A1 (fr) 1975-01-29 1975-01-29 Dispositif de decoupe d'elements structuraux d'un propulseur

Publications (1)

Publication Number Publication Date
FR2299520A1 true FR2299520A1 (fr) 1976-08-27

Family

ID=9150679

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7503339A Withdrawn FR2299520A1 (fr) 1975-01-29 1975-01-29 Dispositif de decoupe d'elements structuraux d'un propulseur

Country Status (1)

Country Link
FR (1) FR2299520A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4840024A (en) * 1984-08-20 1989-06-20 Morton Thiokol, Inc. Multiple propellant solid rocket motor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4840024A (en) * 1984-08-20 1989-06-20 Morton Thiokol, Inc. Multiple propellant solid rocket motor

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Legal Events

Date Code Title Description
ST Notification of lapse