Add to ORKGDesign criteria for integrating electric propulsion system into SERT 2 spacecraft and future spacecraft design
A prototype electric power management and thruster control system for a 30 cm ion thruster is descri...
Electric propulsion (EP) project focused on designing, constructing, testing, and ultimately optimiz...
The topics covered include the following: (1) engine design criteria and issues; (2) design requirem...
Design considerations and requirements for integrating electric propulsion systems into SERT 2 and f...
The SERT C (Space Electric Rocket Test - C) project study defines a spacecraft mission that would de...
The mechanical design of the mercury bombardment thruster that was tested on SERT is described. The ...
The SERT D (Space Electric Rocket Test - D) study defines a possible spacecraft project that would d...
A comparative review of the principles of ion thruster and chemical rocket operations is presented. ...
Because of the current high cost for space experiments on large and small space qualified platforms,...
The objectives of the flight test and a description on how those objectives are in support of an ove...
The directions that electric propulsion technology should take to meet the primary propulsion requir...
Nearly all space missions require on-board propulsion systems and these systems typically have a maj...
The development of electric propulsion systems is discussed and the benefits of these systems to var...
As the Air Force mission in space continues to expand, the cost of delivering the necessary resource...
The NASA Office of Aeronautics, Exploration, and Technology (OAET) supports a research and technolog...
A prototype electric power management and thruster control system for a 30 cm ion thruster is descri...
Electric propulsion (EP) project focused on designing, constructing, testing, and ultimately optimiz...
The topics covered include the following: (1) engine design criteria and issues; (2) design requirem...
Design considerations and requirements for integrating electric propulsion systems into SERT 2 and f...
The SERT C (Space Electric Rocket Test - C) project study defines a spacecraft mission that would de...
The mechanical design of the mercury bombardment thruster that was tested on SERT is described. The ...
The SERT D (Space Electric Rocket Test - D) study defines a possible spacecraft project that would d...
A comparative review of the principles of ion thruster and chemical rocket operations is presented. ...
Because of the current high cost for space experiments on large and small space qualified platforms,...
The objectives of the flight test and a description on how those objectives are in support of an ove...
The directions that electric propulsion technology should take to meet the primary propulsion requir...
Nearly all space missions require on-board propulsion systems and these systems typically have a maj...
The development of electric propulsion systems is discussed and the benefits of these systems to var...
As the Air Force mission in space continues to expand, the cost of delivering the necessary resource...
The NASA Office of Aeronautics, Exploration, and Technology (OAET) supports a research and technolog...
A prototype electric power management and thruster control system for a 30 cm ion thruster is descri...
Electric propulsion (EP) project focused on designing, constructing, testing, and ultimately optimiz...
The topics covered include the following: (1) engine design criteria and issues; (2) design requirem...