Add to ORKGIssued as R & D contract status reports [1-10], and Final report, Project no. E-16-679Final report has title: The fire environment of a solid rocket propellant burning in ai
Issued as Interim scientific report [1-2], and Final scientific report, Project no. E-16-65
Thermal properties and chemical kinetics of solid phase in combustion process of ammonium perchlorat...
Issued as Grant fiscal report, Interim scientific report [1-2], and Final scientific report, Project...
Issued as Interim scientific report, and Final scientific report, Project no. E-16-67
Issued as Progress report, Interim report, and Final report, Project E-16-509Final report has title:...
Flame spreading over surface of igniting solid propellants in different gas mixtures at various pres...
Issued as Interim scientific reports no. [1-3], and Final scientific report, Project no. E-16-632 (c...
Outmoded solid rocket motor propellant is being destroyed by burning as part of the worldwide demili...
Issued as Annual report, Project no. E-16-661 (continued by E-16-673, co-project is E-16-658/Strahle
WOS: 000325647000093The burning rate of the solid rocket propellants is one of the most important fa...
The inclusion of solid propellant plume flow field effects in analyses and design of the space vehic...
A miniature solid propellant rocket motor has been developed to be used in a program to determine th...
Issued as Quarterly progress reports [1-3] and Final report, Project no. E-16-647, School of Aerospa...
Issued as Quarterly reports no. 1-15, Annual report, and Final reports [1-2], Project no. E-16-657Fi...
Heat transfer of solid rocket igniters - flow visualization tests, copper tube firing, and radiant h...
Issued as Interim scientific report [1-2], and Final scientific report, Project no. E-16-65
Thermal properties and chemical kinetics of solid phase in combustion process of ammonium perchlorat...
Issued as Grant fiscal report, Interim scientific report [1-2], and Final scientific report, Project...
Issued as Interim scientific report, and Final scientific report, Project no. E-16-67
Issued as Progress report, Interim report, and Final report, Project E-16-509Final report has title:...
Flame spreading over surface of igniting solid propellants in different gas mixtures at various pres...
Issued as Interim scientific reports no. [1-3], and Final scientific report, Project no. E-16-632 (c...
Outmoded solid rocket motor propellant is being destroyed by burning as part of the worldwide demili...
Issued as Annual report, Project no. E-16-661 (continued by E-16-673, co-project is E-16-658/Strahle
WOS: 000325647000093The burning rate of the solid rocket propellants is one of the most important fa...
The inclusion of solid propellant plume flow field effects in analyses and design of the space vehic...
A miniature solid propellant rocket motor has been developed to be used in a program to determine th...
Issued as Quarterly progress reports [1-3] and Final report, Project no. E-16-647, School of Aerospa...
Issued as Quarterly reports no. 1-15, Annual report, and Final reports [1-2], Project no. E-16-657Fi...
Heat transfer of solid rocket igniters - flow visualization tests, copper tube firing, and radiant h...
Issued as Interim scientific report [1-2], and Final scientific report, Project no. E-16-65
Thermal properties and chemical kinetics of solid phase in combustion process of ammonium perchlorat...
Issued as Grant fiscal report, Interim scientific report [1-2], and Final scientific report, Project...