CH477668A - Spindelförmiges Überschallgeschoss mit Zusatzantrieb durch Heckaufheizung - Google Patents

Spindelförmiges Überschallgeschoss mit Zusatzantrieb durch Heckaufheizung

Info

Publication number
CH477668A
CH477668A CH1813266A CH1813266A CH477668A CH 477668 A CH477668 A CH 477668A CH 1813266 A CH1813266 A CH 1813266A CH 1813266 A CH1813266 A CH 1813266A CH 477668 A CH477668 A CH 477668A
Authority
CH
Switzerland
Prior art keywords
spindle
additional drive
rear heating
supersonic projectile
shaped supersonic
Prior art date
Application number
CH1813266A
Other languages
English (en)
Inventor
Guenter Dipl Ing Ludwig
Original Assignee
Dynamit Nobel 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 Dynamit Nobel Ag filed Critical Dynamit Nobel Ag
Priority to CH1813266A priority Critical patent/CH477668A/de
Priority to SE16827/67A priority patent/SE315533B/xx
Priority to DE19671578225 priority patent/DE1578225A1/de
Priority to GB56887/67A priority patent/GB1173098A/en
Priority to US690539A priority patent/US3545212A/en
Priority to FR1552302D priority patent/FR1552302A/fr
Publication of CH477668A publication Critical patent/CH477668A/de

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/32Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/38Range-increasing arrangements
    • F42B10/42Streamlined projectiles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K7/00Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/14Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines with external combustion, e.g. scram-jet engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/32Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/38Range-increasing arrangements
    • F42B10/40Range-increasing arrangements with combustion of a slow-burning charge, e.g. fumers, base-bleed projectiles

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Carbon And Carbon Compounds (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
CH1813266A 1966-12-15 1966-12-15 Spindelförmiges Überschallgeschoss mit Zusatzantrieb durch Heckaufheizung CH477668A (de)

Priority Applications (6)

Application Number Priority Date Filing Date Title
CH1813266A CH477668A (de) 1966-12-15 1966-12-15 Spindelförmiges Überschallgeschoss mit Zusatzantrieb durch Heckaufheizung
SE16827/67A SE315533B (de) 1966-12-15 1967-12-07
DE19671578225 DE1578225A1 (de) 1966-12-15 1967-12-14 Spindelfoermiges UEberschallgeschoss mit Zusatzantrieb durch Heckaufheizung
GB56887/67A GB1173098A (en) 1966-12-15 1967-12-14 Projectile for Supersonic Flight
US690539A US3545212A (en) 1966-12-15 1967-12-14 Spindle-shaped supersonic projectile with additional propulsion by sternfiring
FR1552302D FR1552302A (de) 1966-12-15 1967-12-15

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH1813266A CH477668A (de) 1966-12-15 1966-12-15 Spindelförmiges Überschallgeschoss mit Zusatzantrieb durch Heckaufheizung

Publications (1)

Publication Number Publication Date
CH477668A true CH477668A (de) 1969-08-31

Family

ID=4430706

Family Applications (1)

Application Number Title Priority Date Filing Date
CH1813266A CH477668A (de) 1966-12-15 1966-12-15 Spindelförmiges Überschallgeschoss mit Zusatzantrieb durch Heckaufheizung

Country Status (6)

Country Link
US (1) US3545212A (de)
CH (1) CH477668A (de)
DE (1) DE1578225A1 (de)
FR (1) FR1552302A (de)
GB (1) GB1173098A (de)
SE (1) SE315533B (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2671452C2 (ru) * 2016-02-24 2018-10-31 Ринад Алиманович Мухамедзянов Гиперзвуковой летательный аппарат

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4170875A (en) * 1976-06-10 1979-10-16 The United States Of America As Represented By The Secretary Of The Air Force Caseless rocket design
GB9001892D0 (en) * 1990-01-26 1990-08-08 Jack Colin A technique for hypervelocity drag reduction by atmospheric heating
US10928168B2 (en) * 2017-11-10 2021-02-23 Curtis E. Graber Noise control system and method for small caliber ammunition

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3008669A (en) * 1955-01-05 1961-11-14 Frank I Tanczos Ramjet missile
US3074668A (en) * 1958-12-10 1963-01-22 Snecma Burner for hot fuel
US3363421A (en) * 1963-01-30 1968-01-16 Gen Applied Science Lab Inc Supersonic engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2671452C2 (ru) * 2016-02-24 2018-10-31 Ринад Алиманович Мухамедзянов Гиперзвуковой летательный аппарат

Also Published As

Publication number Publication date
SE315533B (de) 1969-09-29
FR1552302A (de) 1969-01-03
GB1173098A (en) 1969-12-03
US3545212A (en) 1970-12-08
DE1578225A1 (de) 1971-12-16

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Legal Events

Date Code Title Description
PL Patent ceased