FR2000500A1 - - Google Patents

Info

Publication number
FR2000500A1
FR2000500A1 FR6900969A FR6900969A FR2000500A1 FR 2000500 A1 FR2000500 A1 FR 2000500A1 FR 6900969 A FR6900969 A FR 6900969A FR 6900969 A FR6900969 A FR 6900969A FR 2000500 A1 FR2000500 A1 FR 2000500A1
Authority
FR
France
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Withdrawn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
FR6900969A
Other languages
French (fr)
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of FR2000500A1 publication Critical patent/FR2000500A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B47/00—Compositions in which the components are separately stored until the moment of burning or explosion, e.g. "Sprengel"-type explosives; Suspensions of solid component in a normally non-explosive liquid phase, including a thickened aqueous phase
    • C06B47/02—Compositions in which the components are separately stored until the moment of burning or explosion, e.g. "Sprengel"-type explosives; Suspensions of solid component in a normally non-explosive liquid phase, including a thickened aqueous phase the components comprising a binary propellant
    • C06B47/08—Compositions in which the components are separately stored until the moment of burning or explosion, e.g. "Sprengel"-type explosives; Suspensions of solid component in a normally non-explosive liquid phase, including a thickened aqueous phase the components comprising a binary propellant a component containing hydrazine or a hydrazine derivative
    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B43/00—Compositions characterised by explosive or thermic constituents not provided for in groups C06B25/00 - C06B41/00

Landscapes

  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Catalysts (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
FR6900969A 1968-01-20 1969-01-20 Withdrawn FR2000500A1 (enrdf_load_stackoverflow)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19681646311 DE1646311A1 (de) 1968-01-20 1968-01-20 Feststofftreibsatz fuer kombinierte Raketen-Staustrahltriebwerke und Verfahren zur Herstellung solcher Treibstoffe

Publications (1)

Publication Number Publication Date
FR2000500A1 true FR2000500A1 (enrdf_load_stackoverflow) 1969-09-05

Family

ID=5684575

Family Applications (1)

Application Number Title Priority Date Filing Date
FR6900969A Withdrawn FR2000500A1 (enrdf_load_stackoverflow) 1968-01-20 1969-01-20

Country Status (4)

Country Link
US (1) US3697339A (enrdf_load_stackoverflow)
DE (1) DE1646311A1 (enrdf_load_stackoverflow)
FR (1) FR2000500A1 (enrdf_load_stackoverflow)
GB (1) GB1252497A (enrdf_load_stackoverflow)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4234363A (en) * 1975-07-02 1980-11-18 Rockwell International Corporation Solid propellant hydrogen generator
FR2316204A1 (fr) * 1975-07-03 1977-01-28 Poudres & Explosifs Ste Nale Une composition pyrotechnique eclairante generatrice de gaz
IT8848513A0 (it) * 1987-11-03 1988-10-28 Thiokol Morton Inc Procedimento per preparare propellenti mediante aggiunta posticipata di combustibile metallico
US5811725A (en) * 1996-11-18 1998-09-22 Aerojet-General Corporation Hybrid rocket propellants containing azo compounds
US5917146A (en) * 1997-05-29 1999-06-29 The Regents Of The University Of California High-nitrogen energetic material based pyrotechnic compositions
RU2705058C1 (ru) * 2018-11-12 2019-11-01 Алексей Геннадьевич Ребеко Ракетные топлива на основе сорбитола и перхлоратов натрия и лития
RU2705059C1 (ru) * 2018-11-12 2019-11-01 Алексей Геннадьевич Ребеко Пластификаторы для ракетных топлив на основе сорбитола и перхлората калия
DE102022000497A1 (de) 2021-02-11 2022-08-11 Mathias Herrmann Reaktions- und Auslegungskonzept für Triebwerke zur katalytischen Steuerung / energetischen Auslösung (z.B. mit Metallzusätzen) der inneren Geschwindigkeit (Beschleunigung) und Austrittsgeschwindigkeit mit Beeinflussung von Temperatur sowie Druck für einen verbesserten Wirkungsgrad und Brennraumanpassung (Treiber-Konzept)

Also Published As

Publication number Publication date
DE1646311A1 (de) 1971-07-08
GB1252497A (enrdf_load_stackoverflow) 1971-11-03
US3697339A (en) 1972-10-10

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Legal Events

Date Code Title Description
CD Change of name or company name
ST Notification of lapse