FR2298699A1 - SUPERHEATER THERMAL PUSH MOTOR - Google Patents

SUPERHEATER THERMAL PUSH MOTOR

Info

Publication number
FR2298699A1
FR2298699A1 FR7518763A FR7518763A FR2298699A1 FR 2298699 A1 FR2298699 A1 FR 2298699A1 FR 7518763 A FR7518763 A FR 7518763A FR 7518763 A FR7518763 A FR 7518763A FR 2298699 A1 FR2298699 A1 FR 2298699A1
Authority
FR
France
Prior art keywords
push motor
superheater
thermal push
superheater thermal
motor
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
FR7518763A
Other languages
French (fr)
Other versions
FR2298699B1 (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.)
Northrop Grumman Space and Mission Systems Corp
Original Assignee
TRW Inc
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 TRW Inc filed Critical TRW Inc
Publication of FR2298699A1 publication Critical patent/FR2298699A1/en
Application granted granted Critical
Publication of FR2298699B1 publication Critical patent/FR2298699B1/fr
Granted 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
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/68—Decomposition chambers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/411—Electric propulsion
    • B64G1/415—Arcjets or resistojets
    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06D—MEANS FOR GENERATING SMOKE OR MIST; GAS-ATTACK COMPOSITIONS; GENERATION OF GAS FOR BLASTING OR PROPULSION (CHEMICAL PART)
    • C06D5/00—Generation of pressure gas, e.g. for blasting cartridges, starting cartridges, rockets
    • C06D5/04—Generation of pressure gas, e.g. for blasting cartridges, starting cartridges, rockets by auto-decomposition of single substances

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Organic Chemistry (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physical Or Chemical Processes And Apparatus (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
FR7518763A 1975-01-22 1975-06-16 SUPERHEATER THERMAL PUSH MOTOR Granted FR2298699A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US54319575A 1975-01-22 1975-01-22

Publications (2)

Publication Number Publication Date
FR2298699A1 true FR2298699A1 (en) 1976-08-20
FR2298699B1 FR2298699B1 (en) 1978-02-24

Family

ID=24166979

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7518763A Granted FR2298699A1 (en) 1975-01-22 1975-06-16 SUPERHEATER THERMAL PUSH MOTOR

Country Status (7)

Country Link
JP (1) JPS5950865B2 (en)
CA (1) CA999749A (en)
DE (1) DE2535520C3 (en)
FR (1) FR2298699A1 (en)
GB (1) GB1473749A (en)
IT (1) IT1045168B (en)
NL (1) NL174815C (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2359285A1 (en) * 1976-07-23 1978-02-17 United Kingdom Government ELECTROTHERMAL ROCKET MOTOR
FR2393502A1 (en) * 1976-10-25 1978-12-29 United Kingdom Government PERFECTED ELECTRIC HEATER
FR2411972A1 (en) * 1977-12-14 1979-07-13 Hawker Siddeley Dynamics Ltd Device producing hot fluid stream e.g. hydrazine thruster - has heat shunt upstream of combustion chamber coupled between fuel pipe and heat sink containing fuel valves
FR2510190A1 (en) * 1981-07-21 1983-01-28 Erno Raumfahrttechnik Gmbh PROPELLER ASSEMBLY, IN PARTICULAR FOR SPACE ENGINES

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4305247A (en) * 1979-06-18 1981-12-15 Hughes Aircraft Company Electrothermally augmented hydrazine thruster
US4461144A (en) * 1981-03-19 1984-07-24 The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland Electrothermal gas thrust units
DE3141354C2 (en) * 1981-10-17 1986-12-18 Erno Raumfahrttechnik Gmbh, 2800 Bremen Engine, in particular control engine for spacecraft

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3016693A (en) * 1960-09-23 1962-01-16 John R Jack Electro-thermal rocket
US3210927A (en) * 1963-10-01 1965-10-12 Paul F Brinich Electro-thermal rockets having improved heat exchangers
US3603093A (en) * 1970-03-06 1971-09-07 Nasa Heated porous plug microthrustor

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2359285A1 (en) * 1976-07-23 1978-02-17 United Kingdom Government ELECTROTHERMAL ROCKET MOTOR
FR2393502A1 (en) * 1976-10-25 1978-12-29 United Kingdom Government PERFECTED ELECTRIC HEATER
FR2411972A1 (en) * 1977-12-14 1979-07-13 Hawker Siddeley Dynamics Ltd Device producing hot fluid stream e.g. hydrazine thruster - has heat shunt upstream of combustion chamber coupled between fuel pipe and heat sink containing fuel valves
FR2510190A1 (en) * 1981-07-21 1983-01-28 Erno Raumfahrttechnik Gmbh PROPELLER ASSEMBLY, IN PARTICULAR FOR SPACE ENGINES

Also Published As

Publication number Publication date
NL7505797A (en) 1976-07-26
DE2535520A1 (en) 1976-07-29
FR2298699B1 (en) 1978-02-24
JPS5187610A (en) 1976-07-31
DE2535520C3 (en) 1978-12-07
JPS5950865B2 (en) 1984-12-11
IT1045168B (en) 1980-05-10
DE2535520B2 (en) 1978-04-13
CA999749A (en) 1976-11-16
GB1473749A (en) 1977-05-18
NL174815C (en) 1984-08-16
NL174815B (en) 1984-03-16

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Legal Events

Date Code Title Description
ST Notification of lapse