FR2235284A1 - Propellant block for rockets - with lateral combustion notch and associated flats - Google Patents

Propellant block for rockets - with lateral combustion notch and associated flats

Info

Publication number
FR2235284A1
FR2235284A1 FR7323916A FR7323916A FR2235284A1 FR 2235284 A1 FR2235284 A1 FR 2235284A1 FR 7323916 A FR7323916 A FR 7323916A FR 7323916 A FR7323916 A FR 7323916A FR 2235284 A1 FR2235284 A1 FR 2235284A1
Authority
FR
France
Prior art keywords
block
combustion
notch
flats
lateral
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.)
Granted
Application number
FR7323916A
Other languages
French (fr)
Other versions
FR2235284B1 (en
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 Nationale des Poudres et Explosifs
Original Assignee
Societe Nationale des Poudres et Explosifs
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 Nationale des Poudres et Explosifs filed Critical Societe Nationale des Poudres et Explosifs
Priority to FR7323916A priority Critical patent/FR2235284A1/en
Publication of FR2235284A1 publication Critical patent/FR2235284A1/en
Application granted granted Critical
Publication of FR2235284B1 publication Critical patent/FR2235284B1/fr
Granted 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
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/10Shape or structure of solid propellant charges

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Polyurethanes Or Polyureas (AREA)

Abstract

Propellant blocks, for lateral combustion are partic. intended for rocket propulsion. The block is cylindrical and has a lateral notch parallel to the axis of the block and symmetrical to a diametrical plane of the block; the notch is connected to the external surface by two symmetrical flats. The block has a relative combustion thickness of e/R (in which R is the radius of the block and e the combustion thickness) which can vary between 0.5 and 1.55. The flats lead to a practically constant rate of combustion with a low residual figure, e.g. the amt. of the unburnt portion when the press. is no longer sufficient for normal operation. The blocks can easily be obtd. by moulding a base mixt. of polyurethane resin, potassium perchlorate and ballistic additives. The combustion surface remains constant so that a constant thrust is obtd. throughout the trajectory.
FR7323916A 1973-06-29 1973-06-29 Propellant block for rockets - with lateral combustion notch and associated flats Granted FR2235284A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7323916A FR2235284A1 (en) 1973-06-29 1973-06-29 Propellant block for rockets - with lateral combustion notch and associated flats

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7323916A FR2235284A1 (en) 1973-06-29 1973-06-29 Propellant block for rockets - with lateral combustion notch and associated flats

Publications (2)

Publication Number Publication Date
FR2235284A1 true FR2235284A1 (en) 1975-01-24
FR2235284B1 FR2235284B1 (en) 1976-04-30

Family

ID=9121795

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7323916A Granted FR2235284A1 (en) 1973-06-29 1973-06-29 Propellant block for rockets - with lateral combustion notch and associated flats

Country Status (1)

Country Link
FR (1) FR2235284A1 (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1341801A (en) * 1962-11-29 1963-11-02 Thiokol Chemical Corp Solid rocket propellant powder
US3503334A (en) * 1966-09-30 1970-03-31 Dynamit Nobel Ag Solid propellant charge for rockets

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1341801A (en) * 1962-11-29 1963-11-02 Thiokol Chemical Corp Solid rocket propellant powder
US3503334A (en) * 1966-09-30 1970-03-31 Dynamit Nobel Ag Solid propellant charge for rockets

Also Published As

Publication number Publication date
FR2235284B1 (en) 1976-04-30

Similar Documents

Publication Publication Date Title
CH613500A5 (en) Electrical detonator for detonating the fuel mixture in an internal-combustion engine, especially in a rocket motor
FR2235284A1 (en) Propellant block for rockets - with lateral combustion notch and associated flats
SE7704691L (en) SOLID FUEL WITH COMBUSTION SPEED CATALYST
ES460019A2 (en) Fuel injection pumping apparatus
GB715565A (en) Improvements in or relating to blank ammunition
GB1042737A (en) Improvements in solid propellant rocket motors
GB1371482A (en) Fire-arm ammunition
GB1490511A (en) Solid propelling charge having reinforcing filaments and a method for the production thereof
FR2151495A5 (en) Igniting device for propellant powders - for rocket engines
FR2290409A1 (en) Solid propellant contg uniformly dispersed thin graphite fibres - increasing combustion rate of all propellant types
FR2241696A1 (en) Blocks of solid fuel for rockets - have grooved contour to ensure constant rate of combustion
GB1332905A (en) Solid propellant rocket motors
FR2141004A5 (en) Solid propellant igniter - for rockets with slow burning propellants
HAURY Hydrazinium nitroformate propellant with saturated polymeric hydrocarbon binder(Solid propellant containing hydrazinium nitroformate oxidizer and polymeric hydrocarbon binder)[Patent]
FR2215604A1 (en) Propellant powder block - partic for artillery shells e.g. self-propelled anti-tank shells
FR2016939A1 (en) Solid fuel rockets
VOLK et al. Investigations on the durability of rocket propelling charges(double base rocket propellants, effects of moderators, stabilizers, plastic materials, and environment)[Final Report]
GB941745A (en) A propellent charge containing oxidizer and copolymer
CA886831A (en) Rocket propulsion unit with solid fuel propellant
CA981030A (en) Solid fuel rocket engine
STOKES Comparison of performance of a double-cornered plug nozzle with a conventional convergent-divergent rocket nozzle(Performance comparison of double cornered plug nozzle with conventional convergent-divergent rocket nozzle)
MORGAN Effect of plasticizers on the strength of a plastic motor case(Propellant plasticizer effects on burst strength of glass fiber reinforced plastic motor case)[Final Report]
ES246249A1 (en) Intensive ignition rocking motor with rear and reverse front nozzles. (Machine-translation by Google Translate, not legally binding)
KENDRICK et al. Effects of a magnetic field on burning rate of solid propellant(Magnetic field effects on burning rate of solid rocket propellants)
GB1332910A (en) Rocket type combustion chamber

Legal Events

Date Code Title Description
ST Notification of lapse