[go: up one dir, main page]

GB201517252D0 - Propulsion for aerospace applications - Google Patents

Propulsion for aerospace applications

Info

Publication number
GB201517252D0
GB201517252D0 GBGB1517252.1A GB201517252A GB201517252D0 GB 201517252 D0 GB201517252 D0 GB 201517252D0 GB 201517252 A GB201517252 A GB 201517252A GB 201517252 D0 GB201517252 D0 GB 201517252D0
Authority
GB
United Kingdom
Prior art keywords
propulsion
aerospace applications
aerospace
applications
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.)
Ceased
Application number
GBGB1517252.1A
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.)
LEWIS STEPHEN D
Original Assignee
LEWIS STEPHEN D
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 LEWIS STEPHEN D filed Critical LEWIS STEPHEN D
Priority to GBGB1517252.1A priority Critical patent/GB201517252D0/en
Publication of GB201517252D0 publication Critical patent/GB201517252D0/en
Priority to GB1520441.5A priority patent/GB2542864A/en
Ceased legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06BEXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B47/00Compositions 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
    • C06B47/02Compositions 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
    • C06B47/12Compositions 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 being a liquefied normally gaseous fuel

Landscapes

  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
GBGB1517252.1A 2015-09-30 2015-09-30 Propulsion for aerospace applications Ceased GB201517252D0 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GBGB1517252.1A GB201517252D0 (en) 2015-09-30 2015-09-30 Propulsion for aerospace applications
GB1520441.5A GB2542864A (en) 2015-09-30 2015-11-20 Propulsion for aerospace applications

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB1517252.1A GB201517252D0 (en) 2015-09-30 2015-09-30 Propulsion for aerospace applications

Publications (1)

Publication Number Publication Date
GB201517252D0 true GB201517252D0 (en) 2015-11-11

Family

ID=54544316

Family Applications (2)

Application Number Title Priority Date Filing Date
GBGB1517252.1A Ceased GB201517252D0 (en) 2015-09-30 2015-09-30 Propulsion for aerospace applications
GB1520441.5A Withdrawn GB2542864A (en) 2015-09-30 2015-11-20 Propulsion for aerospace applications

Family Applications After (1)

Application Number Title Priority Date Filing Date
GB1520441.5A Withdrawn GB2542864A (en) 2015-09-30 2015-11-20 Propulsion for aerospace applications

Country Status (1)

Country Link
GB (2) GB201517252D0 (en)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2395113A (en) * 1940-04-01 1946-02-19 Daniel And Florence Guggenheim Mechanism for feeding combustion liquids to rocket apparatus
US3107485A (en) * 1959-05-27 1963-10-22 Ohio Commw Eng Co Propulsion means and method for space vehicles employing a volatile alkene and metalcarbonyl
EP2084394A4 (en) * 2006-11-13 2013-06-19 Space Propulsion Group Inc Mixtures of oxides of nitrogen and oxygen as oxidizers for propulsion, gas generation and power generation applications

Also Published As

Publication number Publication date
GB2542864A (en) 2017-04-05
GB201520441D0 (en) 2016-01-06

Similar Documents

Publication Publication Date Title
IL257811A (en) Fluidic propulsive system
GB2539756B (en) Aircraft propulsion system
GB2537743B (en) Aircraft propulsion system
SG11201610391WA (en) Propulsion system
SG11201610392UA (en) Propulsion system assembly
GB201501045D0 (en) Aircraft propulsion system
SG11201709846PA (en) Ship
GB201508138D0 (en) Aircraft
GB201711060D0 (en) Techniques for sharing applications
GB201616518D0 (en) Aircraft
GB201515279D0 (en) Propulsion system
SG11201710001XA (en) Ship
PL3305649T3 (en) Ship
GB201514901D0 (en) Device for linear propulsion
GB2544400B (en) Propulsion unit for an aircraft
GB2541881B (en) Composite member
PL3305644T3 (en) Ship
IL255065A0 (en) Rudder arrangement
IL243033A0 (en) Rudder system
IL247953A0 (en) Propulsion system
GB2535811B (en) Pre-cooling for aerospace engines
SG11201605286PA (en) Ship
GB201520441D0 (en) Propulsion for aerospace applications
GB201410571D0 (en) Propulsion for aerospace applications
GB2545188B (en) Split hull

Legal Events

Date Code Title Description
AT Applications terminated before publication under section 16(1)