Thesis (M.S.) University of Alaska Fairbanks, 2002Documentation of a comprehensive sounding rocket payload electrical system design methodology is needed by the Alaska Student Rocket Program (ASRP) in order to allow future student designers to build upon the knowledge and experience developed on previous sounding rocket missions, rather than rediscover valuable techniques that were never documented. A systems approach to sounding rocket payload design is presented and supported by a detailed presentation and analysis of the Hawkins/30.047UO 'DIONISYS' (D-region IONIzation measurement SYStem) payload design that was used to measure the D-Region ionization density at high latitudes. Fabrication techniques and test methods that ensure the payl...
voltage in the space environment, (ii) various vacuum breakdown models applied to the space environm...
Current efforts by the student members of the sole student rocket group at Arizona State University,...
Winning poster project completed at Wichita State University, Department of Aerospace Engineering. P...
Thesis (M.S.) University of Alaska Fairbanks, 2003This thesis describes the design and implementatio...
Thesis (M.S.) University of Alaska Fairbanks, 2005This thesis describes the design, development, imp...
Utah State has developed an innovative design for a hybrid thruster to be used in small satellite ap...
Since the spacecraft involved in an experiment conducted in space are relatively expensive, it is ne...
The NASA Undergraduate Student Instrument Project (USIP) is a program with the goal to provide hands...
An overview of a sounding rocket, S-520-25th, project on space tether technology experiment is prese...
A system for controlling the potential of a vehicle (rocket or satellite) in flight by use of an emi...
International Telemetering Conference Proceedings / September 15-17, 1969 / Sheraton Park Hotel, Was...
Thesis (M.S.) University of Alaska Fairbanks, 2007This thesis presents the design and implementation...
Ph.D.Electrical engineeringUniversity of Michigan, Horace H. Rackham School of Graduate Studieshttp:...
A sounding rocket tumble system to enhance deceleration and redirect the flight path angle of a vehi...
We present a design of a small payload for deployment from sounding rockets. The payload is intended...
voltage in the space environment, (ii) various vacuum breakdown models applied to the space environm...
Current efforts by the student members of the sole student rocket group at Arizona State University,...
Winning poster project completed at Wichita State University, Department of Aerospace Engineering. P...
Thesis (M.S.) University of Alaska Fairbanks, 2003This thesis describes the design and implementatio...
Thesis (M.S.) University of Alaska Fairbanks, 2005This thesis describes the design, development, imp...
Utah State has developed an innovative design for a hybrid thruster to be used in small satellite ap...
Since the spacecraft involved in an experiment conducted in space are relatively expensive, it is ne...
The NASA Undergraduate Student Instrument Project (USIP) is a program with the goal to provide hands...
An overview of a sounding rocket, S-520-25th, project on space tether technology experiment is prese...
A system for controlling the potential of a vehicle (rocket or satellite) in flight by use of an emi...
International Telemetering Conference Proceedings / September 15-17, 1969 / Sheraton Park Hotel, Was...
Thesis (M.S.) University of Alaska Fairbanks, 2007This thesis presents the design and implementation...
Ph.D.Electrical engineeringUniversity of Michigan, Horace H. Rackham School of Graduate Studieshttp:...
A sounding rocket tumble system to enhance deceleration and redirect the flight path angle of a vehi...
We present a design of a small payload for deployment from sounding rockets. The payload is intended...
voltage in the space environment, (ii) various vacuum breakdown models applied to the space environm...
Current efforts by the student members of the sole student rocket group at Arizona State University,...
Winning poster project completed at Wichita State University, Department of Aerospace Engineering. P...