Add to ORKGIssued as Interim scientific reports no. [1-3], and Final scientific report, Project no. E-16-632 (co-projects are: E-16-634/E. W. Price; E-16-635/W. C. Strahle; E-16-637/B. T. Zinn)Title on spine: Rocket research at Georgia TechProject no. E-16-634 has title: Behavior of aluminum in combustion of solid rocket propellantsProject no. E-16-635 has title: Rocket motor aeroacousticsProject no. E-16-637 has title: Solid propellant response factor measuremen
Solid Rocket Motors (SRMs) are used across a variety of platforms from aircraft missiles to space sh...
Design, testing, and development of solid propellant rocket engine for orbital transfer of Applicati...
The Eagle Space Flight Team was created with the goal of becoming the first undergraduate team to de...
Issued as Interim scientific report, and Final scientific report, Project no. E-16-67
Issued as R & D contract status reports [1-10], and Final report, Project no. E-16-679Final report h...
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
Issued as Interim scientific report [1-2], and Final scientific report, Project no. E-16-65
Issued as Progress report no. 1, Interim scientific reports no. 2-3, and Final scientific report, Pr...
The project\u27s primary goal is to research, design, and manufacture solid rocket motors for compet...
The research team will take an existing student-developed solid rocket propellant, refine its formul...
Issued as Semi-annual report, Annual report, and Contractor report, Project no. E-16-635Contractor r...
The use of solid propellant motors has been around since the early days of rocketry, with applicatio...
A miniature solid propellant rocket motor has been developed to be used in a program to determine th...
Solid Rocket Motors (SRMs) are used across a variety of platforms from aircraft missiles to space sh...
Design, testing, and development of solid propellant rocket engine for orbital transfer of Applicati...
The Eagle Space Flight Team was created with the goal of becoming the first undergraduate team to de...
Issued as Interim scientific report, and Final scientific report, Project no. E-16-67
Issued as R & D contract status reports [1-10], and Final report, Project no. E-16-679Final report h...
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
Issued as Interim scientific report [1-2], and Final scientific report, Project no. E-16-65
Issued as Progress report no. 1, Interim scientific reports no. 2-3, and Final scientific report, Pr...
The project\u27s primary goal is to research, design, and manufacture solid rocket motors for compet...
The research team will take an existing student-developed solid rocket propellant, refine its formul...
Issued as Semi-annual report, Annual report, and Contractor report, Project no. E-16-635Contractor r...
The use of solid propellant motors has been around since the early days of rocketry, with applicatio...
A miniature solid propellant rocket motor has been developed to be used in a program to determine th...
Solid Rocket Motors (SRMs) are used across a variety of platforms from aircraft missiles to space sh...
Design, testing, and development of solid propellant rocket engine for orbital transfer of Applicati...
The Eagle Space Flight Team was created with the goal of becoming the first undergraduate team to de...