The retarding ion mass spectrometer (RIMS) for Dynamics Explorer-1 is an instrument designed to measure the details of the thermal plasma distribution. It combines the ion temperature determining capability of the retarding potential analyzer with the compositional capabilities of the mass spectrometer and adds multiple sensor heads to sample all directions relative to the spacecraft ram direction. This manual provides a functional description of the RIMS, the instrument calibration, and a description of the commands which can be stored in the instrument logic to control its operation
Rocket borne mass spectrometer measurements of positive ion composition in ionospher
The development of flight suitable analyzer units for that part of the GIOTTO Ion Mass Spectrometer ...
This final technical report covers the activities engaged in by the University of Texas at Dallas, C...
The Retarding Ion Mass Spectrometer (RIMS) on the Dynamics Explorer 1 spacecraft observes both the t...
The Retarding Ion Mass Spectrometer (RIMS) experiment onboard the Dynamics Explorer 1 (DE 1) satelli...
Activities of the RIMS instrument during the extended mission are planned. The modes of operation fo...
The retarding ion mass spectrometer (RIMS) experiment onboard the Dynamics Explorer 1 (DE 1) satelli...
The retarding ion mass spectrometer (RIMS) experiment onboard the Dynamics Explorer 1 (DE 1) satelli...
Data from a sounding rocket flight of the swept angle retarding ion mass spectrometer (SARIMS) are p...
The retarding potential analyzer and drift meter were carried aboard all three Atmosphere Explorer s...
The Retarding Ion Mass Spectrometer (RIMS) on the Dynamics Explorer 1 (DE 1) satellite has provided ...
Operating and maintenance instructions for experimental nonmagnetic flight mass spectromete
The ion drift meter for Dynamics Explorer B is discussed. It measures two mutually perpendicular ang...
Analysis techniques and software development; data analysis and modeling; spacecraft sheath effects;...
The University of Texas at Dallas (UTD) Center for Space Sciences (CSS) has designed, developed, and...
Rocket borne mass spectrometer measurements of positive ion composition in ionospher
The development of flight suitable analyzer units for that part of the GIOTTO Ion Mass Spectrometer ...
This final technical report covers the activities engaged in by the University of Texas at Dallas, C...
The Retarding Ion Mass Spectrometer (RIMS) on the Dynamics Explorer 1 spacecraft observes both the t...
The Retarding Ion Mass Spectrometer (RIMS) experiment onboard the Dynamics Explorer 1 (DE 1) satelli...
Activities of the RIMS instrument during the extended mission are planned. The modes of operation fo...
The retarding ion mass spectrometer (RIMS) experiment onboard the Dynamics Explorer 1 (DE 1) satelli...
The retarding ion mass spectrometer (RIMS) experiment onboard the Dynamics Explorer 1 (DE 1) satelli...
Data from a sounding rocket flight of the swept angle retarding ion mass spectrometer (SARIMS) are p...
The retarding potential analyzer and drift meter were carried aboard all three Atmosphere Explorer s...
The Retarding Ion Mass Spectrometer (RIMS) on the Dynamics Explorer 1 (DE 1) satellite has provided ...
Operating and maintenance instructions for experimental nonmagnetic flight mass spectromete
The ion drift meter for Dynamics Explorer B is discussed. It measures two mutually perpendicular ang...
Analysis techniques and software development; data analysis and modeling; spacecraft sheath effects;...
The University of Texas at Dallas (UTD) Center for Space Sciences (CSS) has designed, developed, and...
Rocket borne mass spectrometer measurements of positive ion composition in ionospher
The development of flight suitable analyzer units for that part of the GIOTTO Ion Mass Spectrometer ...
This final technical report covers the activities engaged in by the University of Texas at Dallas, C...