Fuel Regression Characteristics in Hybrid Rockets Using Nitrous Oxide/High-Density Polyethylene


Hokkaido University \| Library \| HUSCAP	Advanced Search		言語

	Home
	About HUSCAP
	Open Access Policy

	Browse by Author

Browse
	Communities & Collections

	Scholarly Journals
	Theses
	Doctoral Dissertations Listed by Graduate Schools
	Conference Procs.
	Events

	HUSCAP Senior (in Japanese)

	Societies

	Downloads (country)

For university staff
	How to post your papers to HUSCAP
	Publication of theses
	Helpline about theses publication

Open Archives Compliant

You can search our collection also at:
	Google
	Google Scholar
	CiNii
	IRDB
	OAIster
	NDLTD

Files in This Item:

JPP_for_submittion.pdf

799.88 kB

PDF

Please use this identifier to cite or link to this item:http://hdl.handle.net/2115/81670

Title:	Fuel Regression Characteristics in Hybrid Rockets Using Nitrous Oxide/High-Density Polyethylene
Authors:	Ito, Seiji Browse this author
	Kamps, Landon Browse this author
	Nagata, Harunori Browse this author →KAKEN DB
Issue Date:	Mar-2021
Publisher:	The American Institute of Aeronautics and Astronautics
Journal Title:	Journal of propulsion and power
Volume:	37
Issue:	2
Start Page:	342
End Page:	348
Publisher DOI:	10.2514/1.B37875
Type:	article (author version)
URI:	http://hdl.handle.net/2115/81670
Appears in Collections:	工学院・工学研究院 (Graduate School of Engineering / Faculty of Engineering) > 雑誌発表論文等 (Peer-reviewed Journal Articles, etc)

Submitter: 永田晴紀

OAI-PMH ( junii2 , jpcoar_1.0 )

- Hokkaido University