The ISARA mission is a technology demonstration of a practical, low cost Ka-band High Gain Antenna (HGA) on a 3U CubeSat that will enable 100 Mbps downlink data with minimal impact on spacecraft mass, volume, cost and power requirements. The key to this technical advance is the integration of a reflectarray HGA into a Pumpkin PMDSAS Turkey Tail solar array. ISARA will fly a nominal 5 month mission that demonstrates the technology on orbit. This paper presents an overview of the ISARA CubeSat mission with emphasis on the unique antenna / solar panel design and a description of the mission design that will verify the antenna performance and validate the data rate capability
Master's Project (M.S.) University of Alaska Fairbanks, 2017Power budgets on small satellites are re...
Over the past several years, technology and launch opportunities for CubeSats have exploded, enablin...
This paper describes the design of an antenna array of microstrip patches for CubeSats o...
The Integrated Solar Array and Reflectarray Antenna (ISARA) mission will demonstrate a reflectarray ...
The goal of the Integrated Solar-Panel Antenna Array for CubeSats (ISAAC) project is to design and d...
Integrated Solar-Panel Antenna Array for CubeSats (ISAAC) is a high gain, efficient, lightweight, co...
With an increasing presence among educational, commercial and governmental agencies, CubeSats are on...
The advent of VLSI and microelectronics has made it possible to reduce the size of electronic device...
The paper reports the latest development of a clear solution for CubeSat antennas where an X band op...
A CubeSat is a very small satellite that has been achieving growing interests in space exploration. ...
CubeSats are a type of small satellites (< 500 kg) that weigh several kilograms and consist of multi...
CubeSats are a miniaturized class of satellites that are launched as secondary payloads, offering th...
Antennas conformal to a Cubesat surface have many advantages compared to deployed antennas. This stu...
CubeSats are a class of miniaturized satellites that have become increasingly popular in academia an...
The F10.7 solar flux index is a measure of microwave solar emissions at a wavelength of 10.7 cm or 2...
Master's Project (M.S.) University of Alaska Fairbanks, 2017Power budgets on small satellites are re...
Over the past several years, technology and launch opportunities for CubeSats have exploded, enablin...
This paper describes the design of an antenna array of microstrip patches for CubeSats o...
The Integrated Solar Array and Reflectarray Antenna (ISARA) mission will demonstrate a reflectarray ...
The goal of the Integrated Solar-Panel Antenna Array for CubeSats (ISAAC) project is to design and d...
Integrated Solar-Panel Antenna Array for CubeSats (ISAAC) is a high gain, efficient, lightweight, co...
With an increasing presence among educational, commercial and governmental agencies, CubeSats are on...
The advent of VLSI and microelectronics has made it possible to reduce the size of electronic device...
The paper reports the latest development of a clear solution for CubeSat antennas where an X band op...
A CubeSat is a very small satellite that has been achieving growing interests in space exploration. ...
CubeSats are a type of small satellites (< 500 kg) that weigh several kilograms and consist of multi...
CubeSats are a miniaturized class of satellites that are launched as secondary payloads, offering th...
Antennas conformal to a Cubesat surface have many advantages compared to deployed antennas. This stu...
CubeSats are a class of miniaturized satellites that have become increasingly popular in academia an...
The F10.7 solar flux index is a measure of microwave solar emissions at a wavelength of 10.7 cm or 2...
Master's Project (M.S.) University of Alaska Fairbanks, 2017Power budgets on small satellites are re...
Over the past several years, technology and launch opportunities for CubeSats have exploded, enablin...
This paper describes the design of an antenna array of microstrip patches for CubeSats o...