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Method Article

Improving the Combustion Performance of a Hybrid Rocket Engine using a Novel Fuel Grain with a Nested Helical Structure

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DOI:

10.3791/61555

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January 18th, 2021

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In This Article

Summary

A technique utilizing a solid fuel grain with a novel nested helical structure to improve the combustion performance of a hybrid rocket engine is presented.

Abstract

A technique to improve the combustion performance of a hybrid rocket engine using a novel fuel grain structure is presented. This technique utilizes the different regression rates of acrylonitrile butadiene styrene and paraffin-based fuels, which increase the exchanges of both matter and energy by swirl flow and recirculation zones formed at the grooves between the adjacent vanes. The centrifugal casting technique is used to cast the paraffin-based fuel into an acrylonitrile butadiene styrene substrate made by three-dimensional printing. Using oxygen as the oxidizer, a series of tests were conducted to investigate the combustion performance of the novel fuel grain. In comparison to paraffin-based fuel grains, the fuel grain with a nested helical structure, which can be maintained throughout the combustion process, showed significant improvement in the regression rate and great potential in improvement of combustion efficiency.

Introduction

A technique to improve the combustion performance of a hybrid rocket engine is urgently required. To date, practical applications of hybrid rocket engines are still far less than those of solid and liquid rocket engines1,2. The low regression rate of traditional fuels limits the improvement of thrust performance for the hybrid rocket engine3,4. In addition, its combustion efficiency is slightly lower than that of other chemical energy rockets due to internal diffusion combustion5, as shown in Figure 1

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Protocol

1. Experimental setup and procedures

  1. Preparation of fuel grain
    NOTE: The fuel grain with novel structure consisted of two parts, which are shown in Figure 4. As the main part of the novel grain, the paraffin-based fuel accounts for more than 80% of the total mass. The ABS substrate is used as an additional fuel. The preparation of this fuel grain was realized by combining 3D printing and centrifugal casting.
    1. Substrate preparation
      1. Open 3D software for ABS substrate drawing.
        NOTE: The ABS substrate, which intended to provide the helical framework and support for the paraffin-based fuel, is c....

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Results

Figure 7 shows the changes in combustion chamber pressure and oxidizer mass flow rate. To provide the necessary time for flow regulation, the oxidizer enters the combustion chamber in advance. When the engine builds pressure in the combustion chamber, the oxygen mass flow rate drops rapidly and then maintains a relatively steady change. During the combustion process, the pressure in the combustion chamber remains relatively stable.

Images showing a comparison of c.......

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Discussion

The technique presented in this paper is a novel approach using a fuel grain with a nested helical structure. There are no difficulties in setting up the necessary equipment and facilities. The helical structure can be easily produced by 3D printing, and nesting of paraffin-based fuels can be easily carried out by centrifugal casting. Fused deposition molding (FDM) 3D printers are not expensive and the cost of centrifuges is low.

When the inner surface of the shaped fuel grain was found to hav.......

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Disclosures

The authors have nothing to disclose.

Acknowledgements

This work was supported by the National Natural Science Foundation of China (Grant Nos. 11802315, 11872368 and 11927803) and Equipment Pre-Research Foundation of National Defense Key Laboratory (Grant No. 6142701190402).

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Materials

List of materials used in this article
NameCompanyCatalog NumberComments
3D printerRaise3DN2 Plus305 × 305 × 605 mm
3D drawing softwareAutodeskInventor
ABSRaise3DABS black1.75 mm
CameraSonyA6000
CarbonAibeisiATP-88AT
Centrifugal machineLuqiao Langbo Motor Co.LtdCustom≤1450 rpm
Data processing softwareOriginLabOrigin 2020
EVADuPont Company360binder
Mass flow controllerBronkhostF-203AV0-1500 ln/min
Melt mixerWinzhou Chengyi Jixie Co.LtdCustom
Multi-function data acquisition cardNIUSB-6211
ParaffinSinopec Group Company58#Fully refined paraffin, Melting point≈58°C
PE waxQatar petroleum chemical industry CompanyCustom
Slicing softwareRaise3DideaMaker
Spark plugNGKPFR7S8EG
Stearic acidical Reagent CompanyCustomhardener

References

  1. Boiron, A. J., Cantwell, B. 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. , (2013).
  2. Mazzetti, A., Merotto, L., Pinarello, G. Paraffin-based hybrid rocket engines applications: A review and a market perspective. Acta Astronautica. 126, 286-297 (2016).
  3. K....

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Fuel Grain StructureABS SubstrateParaffin-Based FuelCentrifugal Casting3D PrintingRegression RateOxidizer Mass Flow Rate