CN103834445A - Fuel - Google Patents

Fuel Download PDF

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Publication number
CN103834445A
CN103834445A CN201310643762.9A CN201310643762A CN103834445A CN 103834445 A CN103834445 A CN 103834445A CN 201310643762 A CN201310643762 A CN 201310643762A CN 103834445 A CN103834445 A CN 103834445A
Authority
CN
China
Prior art keywords
fuel
rocket
ether
aluminum hydride
density
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.)
Pending
Application number
CN201310643762.9A
Other languages
Chinese (zh)
Inventor
杨贻方
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.)
Suzhou Niuwu Erguan Electrical Appliance Science & Technology Co Ltd
Original Assignee
Suzhou Niuwu Erguan Electrical Appliance Science & Technology Co 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 Suzhou Niuwu Erguan Electrical Appliance Science & Technology Co Ltd filed Critical Suzhou Niuwu Erguan Electrical Appliance Science & Technology Co Ltd
Priority to CN201310643762.9A priority Critical patent/CN103834445A/en
Publication of CN103834445A publication Critical patent/CN103834445A/en
Pending legal-status Critical Current

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Abstract

The invention provides fuel. The fuel comprises 26-35wt% of aluminum trihydride and 65-74wt% of ethyl ether. Aluminum trihydride is high-energy fuel, can be dissolved in ethyl ether and can greatly improve fuel density to more than 1.5g/cm<3> so that a rocket volume is reduced effectively and emission payload is improved and thus the fuel is suitable for emission of 150-1500t of a rocket and can be used for space station construction and civil space motion.

Description

A kind of fuel
Technical field
The present invention relates to a kind of fuel, especially rocket fuel.
Background technology
Rocket engine is the one of jet engine, and the reactant in propellant tank or launch vehicle (propelling agent) is become to high-speed jet, because newton's second law of motion produces thrust.Rocket engine can be used for spacecraft propulsion, also can be used for guided missile etc. and flies in endoatmosphere.
Current most of rocket engine is all to adopt liquid fuel, and the specific impulse of solid is little, but the density of liquid fuel is smaller at present, picture kerosene etc., density is at 0.84 gram/cc, and density is little like this can increase kerosene hold-up vessel volume, thus entire effect rocket load.
Summary of the invention
The invention provides a kind of highdensity rocket fuel.
Technical scheme is as follows:
A kind of fuel, is characterized in that being made up of ether and three aluminum hydride, and wherein three aluminum hydride content are 26~35wt%, and ether is 65~74% wt%.
Because three aluminum hydride are also high energy fuels, can dissolve in ether like this, more than can increasing considerably the density to 1.5 gram/cc of fuel, thereby reduce rocket volume, improve transmitting workload.
Embodiment
In concrete enforcement, there are multiple implementation details and prioritization scheme:
1. while making, three aluminum hydride are dissolved in ether, mixture is kept to-10 degrees Celsius of following low temperature.
2. in fuel, suitably add aluminium powder.
The rocket launching that is suitable for 150~1500 tons of the present invention, builds and civilian space activity for space station.

Claims (3)

1. a fuel, is characterized in that being made up of ether and three aluminum hydride, and wherein three aluminum hydride content are 26~35wt%, and ether is 65~74% wt%.
2. a kind of fuel according to claim 1, is dissolved in three aluminum hydride in ether while it is characterized in that making, and mixture is kept to-10 degrees Celsius of following low temperature.
3. a kind of fuel according to claim 1, is characterized in that suitably adding aluminium powder in fuel.
CN201310643762.9A 2013-12-05 2013-12-05 Fuel Pending CN103834445A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310643762.9A CN103834445A (en) 2013-12-05 2013-12-05 Fuel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310643762.9A CN103834445A (en) 2013-12-05 2013-12-05 Fuel

Publications (1)

Publication Number Publication Date
CN103834445A true CN103834445A (en) 2014-06-04

Family

ID=50798346

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310643762.9A Pending CN103834445A (en) 2013-12-05 2013-12-05 Fuel

Country Status (1)

Country Link
CN (1) CN103834445A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109694759A (en) * 2019-03-07 2019-04-30 西安近代化学研究所 A kind of punching engine slurry fuel

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109694759A (en) * 2019-03-07 2019-04-30 西安近代化学研究所 A kind of punching engine slurry fuel

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Legal Events

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C06 Publication
PB01 Publication
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20140604