Title:
高分子量ジオールを有するヒドロキシル基末端バインダを備えた固体ロケットモータ
Document Type and Number:
Japanese Patent JP6735345
Kind Code:
B2
Abstract:
A solid rocket propellant includes a hydroxyl-terminated polybudadiene (HTPB) binder system having a high molecular weight diol that is greater than thirty carbon atoms (>C30) and less than fifty carbon atoms (
Inventors:
Doll, daniel
Dolly, Scott K.
Dolly, Scott K.
Application Number:
JP2018524797A
Publication Date:
August 05, 2020
Filing Date:
November 15, 2016
Export Citation:
Assignee:
AeroJet Rocket Dyne Incorporated
International Classes:
C06D5/00; C06B23/00; C06B27/00; C06B29/02; C06B29/22
Domestic Patent References:
| JP62256784A | ||||
| JP2002527337A |
Foreign References:
| US4210474 |
Attorney, Agent or Firm:
Hiromichi Kobayashi
Tomioka Kiyoshi
Tomioka Kiyoshi