Work

Experimental investigation of fuel regression rate in a HTPB based lab-scale hybrid rocket motor

Year: 2014

Type: article

Source: Acta Astronautica

DOI: 10.1016/j.actaastro.2014.08.028

Authors: Xintian Li, Hui Tian, Nanjia Yu, Guobiao Cai

Institution: Beihang University

Language: English

Topic: Rocket and propulsion systems research

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W2014697366

FWCI: 3.423

Cites: 15

Cited by: 40

Related to: 10