Add to ORKGThis report presents the results obtained during the past year in a research program on Solid Propel...
Issued as Research proposal and Annual scientific report, Project no. E-19-636 (continuation of E-19...
of aluminum particle ignition behavior in open atmosphere rocket propellant fires Nadir Yilmaz The s...
Issued as Interim scientific reports no. [1-3], and Final scientific report, Project no. E-16-632 (c...
Issued as R & D contract status reports [1-10], and Final report, Project no. E-16-679Final report h...
Issued as Quarterly report 1-13, and Annual summary report 1-2, Project no. E-16-62
Issued as Quarterly reports no. 1-15, Annual report, and Final reports [1-2], Project no. E-16-657Fi...
WOS: 000325647000093The burning rate of the solid rocket propellants is one of the most important fa...
Issued as Progress report, Interim report, and Final report, Project E-16-509Final report has title:...
Issued as Annual report, Project no. E-16-661 (continued by E-16-673, co-project is E-16-658/Strahle
Energetic materials have been widely used for military purposes. Continuous research programs are pe...
Issued as Interim scientific report [1-2], and Final scientific report, Project no. E-16-65
Alumina size distributions were obtained for both a coarse and a fine oxidizer composite propellant ...
Issued as Monthly progress reports [nos. 1-13], Report, Draft Final report, and Final report, Projec...
Aluminized composite propellant used in solid rocket motors contain a lot of aluminium particles bec...
This report presents the results obtained during the past year in a research program on Solid Propel...
Issued as Research proposal and Annual scientific report, Project no. E-19-636 (continuation of E-19...
of aluminum particle ignition behavior in open atmosphere rocket propellant fires Nadir Yilmaz The s...
Issued as Interim scientific reports no. [1-3], and Final scientific report, Project no. E-16-632 (c...
Issued as R & D contract status reports [1-10], and Final report, Project no. E-16-679Final report h...
Issued as Quarterly report 1-13, and Annual summary report 1-2, Project no. E-16-62
Issued as Quarterly reports no. 1-15, Annual report, and Final reports [1-2], Project no. E-16-657Fi...
WOS: 000325647000093The burning rate of the solid rocket propellants is one of the most important fa...
Issued as Progress report, Interim report, and Final report, Project E-16-509Final report has title:...
Issued as Annual report, Project no. E-16-661 (continued by E-16-673, co-project is E-16-658/Strahle
Energetic materials have been widely used for military purposes. Continuous research programs are pe...
Issued as Interim scientific report [1-2], and Final scientific report, Project no. E-16-65
Alumina size distributions were obtained for both a coarse and a fine oxidizer composite propellant ...
Issued as Monthly progress reports [nos. 1-13], Report, Draft Final report, and Final report, Projec...
Aluminized composite propellant used in solid rocket motors contain a lot of aluminium particles bec...
This report presents the results obtained during the past year in a research program on Solid Propel...
Issued as Research proposal and Annual scientific report, Project no. E-19-636 (continuation of E-19...
of aluminum particle ignition behavior in open atmosphere rocket propellant fires Nadir Yilmaz The s...