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ES186161U - Rocket motor. (Machine-translation by Google Translate, not legally binding) - Google Patents

Rocket motor. (Machine-translation by Google Translate, not legally binding)

Info

Publication number
ES186161U
ES186161U ES0186161U ES186161U ES186161U ES 186161 U ES186161 U ES 186161U ES 0186161 U ES0186161 U ES 0186161U ES 186161 U ES186161 U ES 186161U ES 186161 U ES186161 U ES 186161U
Authority
ES
Spain
Prior art keywords
translation
machine
legally binding
google translate
rocket 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
ES0186161U
Other languages
Spanish (es)
Other versions
ES186161Y (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.)
Imperial Chemical Industries Ltd
Original Assignee
Imperial Chemical Industries Ltd
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 Imperial Chemical Industries Ltd filed Critical Imperial Chemical Industries Ltd
Priority to ES1972186161U priority Critical patent/ES186161Y/en
Publication of ES186161U publication Critical patent/ES186161U/en
Application granted granted Critical
Publication of ES186161Y publication Critical patent/ES186161Y/en
Expired legal-status Critical Current

Links

Landscapes

  • Application Of Or Painting With Fluid Materials (AREA)
  • Solid Fuels And Fuel-Associated Substances (AREA)

Abstract

Motor de cohete caracterizado porque la superficie externa de la tobera de motor de cohete y/o la superficie de una prolongación de le tobera lleva un revestimiento de un material capaz de arder a la temperatura que alcanza la tobera y/o la prolongación durante el funcionamiento del motor.Rocket engine characterized in that the outer surface of the rocket engine nozzle and / or the surface of an extension of the nozzle is coated with a material capable of burning at the temperature reached by the nozzle and / or the extension during operation. the motor.

ES1972186161U 1972-11-28 1972-11-28 ROCKET ENGINE. Expired ES186161Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES1972186161U ES186161Y (en) 1972-11-28 1972-11-28 ROCKET ENGINE.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES1972186161U ES186161Y (en) 1972-11-28 1972-11-28 ROCKET ENGINE.

Publications (2)

Publication Number Publication Date
ES186161U true ES186161U (en) 1973-10-16
ES186161Y ES186161Y (en) 1974-07-01

Family

ID=8358000

Family Applications (1)

Application Number Title Priority Date Filing Date
ES1972186161U Expired ES186161Y (en) 1972-11-28 1972-11-28 ROCKET ENGINE.

Country Status (1)

Country Link
ES (1) ES186161Y (en)

Also Published As

Publication number Publication date
ES186161Y (en) 1974-07-01

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