Add to ORKGDesign considerations and requirements for integrating electric propulsion systems into SERT 2 and future spacecraf
The objectives of the flight test and a description on how those objectives are in support of an ove...
A comparative review of the principles of ion thruster and chemical rocket operations is presented. ...
A set of missions was postulated that was considered to be representative of those likely to be desi...
Design criteria for integrating electric propulsion system into SERT 2 spacecraft and future spacecr...
The SERT C (Space Electric Rocket Test - C) project study defines a spacecraft mission that would de...
Nearly all space missions require on-board propulsion systems and these systems typically have a maj...
The mechanical design of the mercury bombardment thruster that was tested on SERT is described. The ...
The directions that electric propulsion technology should take to meet the primary propulsion requir...
The NASA Office of Aeronautics, Exploration, and Technology (OAET) supports a research and technolog...
The SERT D (Space Electric Rocket Test - D) study defines a possible spacecraft project that would d...
The development of electric propulsion systems is discussed and the benefits of these systems to var...
Development and characteristics of electric propulsion systems for manned and unmanned spacecraf
Most space missions require on-board propulsion systems and these systems are often dominant spacecr...
Because of the current high cost for space experiments on large and small space qualified platforms,...
A functional matrix of possible propulsion system characteristics for a spacecraft for deployable an...
The objectives of the flight test and a description on how those objectives are in support of an ove...
A comparative review of the principles of ion thruster and chemical rocket operations is presented. ...
A set of missions was postulated that was considered to be representative of those likely to be desi...
Design criteria for integrating electric propulsion system into SERT 2 spacecraft and future spacecr...
The SERT C (Space Electric Rocket Test - C) project study defines a spacecraft mission that would de...
Nearly all space missions require on-board propulsion systems and these systems typically have a maj...
The mechanical design of the mercury bombardment thruster that was tested on SERT is described. The ...
The directions that electric propulsion technology should take to meet the primary propulsion requir...
The NASA Office of Aeronautics, Exploration, and Technology (OAET) supports a research and technolog...
The SERT D (Space Electric Rocket Test - D) study defines a possible spacecraft project that would d...
The development of electric propulsion systems is discussed and the benefits of these systems to var...
Development and characteristics of electric propulsion systems for manned and unmanned spacecraf
Most space missions require on-board propulsion systems and these systems are often dominant spacecr...
Because of the current high cost for space experiments on large and small space qualified platforms,...
A functional matrix of possible propulsion system characteristics for a spacecraft for deployable an...
The objectives of the flight test and a description on how those objectives are in support of an ove...
A comparative review of the principles of ion thruster and chemical rocket operations is presented. ...
A set of missions was postulated that was considered to be representative of those likely to be desi...