GB1173098A - Projectile for Supersonic Flight - Google Patents

Projectile for Supersonic Flight

Info

Publication number
GB1173098A
GB1173098A GB56887/67A GB5688767A GB1173098A GB 1173098 A GB1173098 A GB 1173098A GB 56887/67 A GB56887/67 A GB 56887/67A GB 5688767 A GB5688767 A GB 5688767A GB 1173098 A GB1173098 A GB 1173098A
Authority
GB
United Kingdom
Prior art keywords
missile
indicated
supersonic
frusto
dec
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.)
Expired
Application number
GB56887/67A
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.)
FINANC D EXPANSION COMMERCIAL
Original Assignee
FINANC D EXPANSION COMMERCIAL
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 FINANC D EXPANSION COMMERCIAL filed Critical FINANC D EXPANSION COMMERCIAL
Publication of GB1173098A publication Critical patent/GB1173098A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means 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
    • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/38—Range-increasing arrangements
    • F42B10/42—Streamlined projectiles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants 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
    • F02K7/10—Plants 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
    • F02K7/14—Plants 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means 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
    • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/38—Range-increasing arrangements
    • F42B10/40—Range-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)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
  • Carbon And Carbon Compounds (AREA)

Abstract

1,173,098. Supersonic missile. SOC. FINANCIERE D'EXPANSION COMMERCIAL ET INDUSTRIELLE S. A. Dec. 14, 1967 [Dec. 15, 1966], No. 56887/ 67. Heading F1J. The invention relates to a supersonic missile in which fuel is discharged externally of the missile body and burns downstream of a shock wave so producing thrust on the missile. The missile is pointed at its forward and rearward ends, there being a frusto-conical surface 3 of increasing diameter in the downstream direction, disposed in the region of largest diameter. Adjacent the upstream end of the frusto-conical surface are disposed fuel ejection openings 2. The shock wave created at the forward end of the missile is indicated at 1 and that created at the surface 3 is indicated at 4. The rearward portion of the missile may be of curved convergent form as indicated in full lines or of conical form as indicated by broken lines.
GB56887/67A 1966-12-15 1967-12-14 Projectile for Supersonic Flight Expired GB1173098A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH1813266A CH477668A (en) 1966-12-15 1966-12-15 Spindle-shaped supersonic projectile with additional drive through rear heating

Publications (1)

Publication Number Publication Date
GB1173098A true GB1173098A (en) 1969-12-03

Family

ID=4430706

Family Applications (1)

Application Number Title Priority Date Filing Date
GB56887/67A Expired GB1173098A (en) 1966-12-15 1967-12-14 Projectile for Supersonic Flight

Country Status (6)

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

Families Citing this family (4)

* 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
RU2671452C2 (en) * 2016-02-24 2018-10-31 Ринад Алиманович Мухамедзянов Hypersonic aircraft
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

Also Published As

Publication number Publication date
FR1552302A (en) 1969-01-03
CH477668A (en) 1969-08-31
SE315533B (en) 1969-09-29
US3545212A (en) 1970-12-08
DE1578225A1 (en) 1971-12-16

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PLNP Patent lapsed through nonpayment of renewal fees