151. A Deployable High-Gain Antenna Bound for Mars: Developing a new folded-panel reflectarray for the first CubeSat mission to Mars
- Author
-
Richard Hodges, Daniel J. Hoppe, Joseph D. Vacchione, and Nacer Chahat
- Subjects
Engineering ,Directional antenna ,Spacecraft ,business.industry ,Payload ,020208 electrical & electronic engineering ,020206 networking & telecommunications ,02 engineering and technology ,Mars Exploration Program ,Condensed Matter Physics ,USable ,Stowage ,0202 electrical engineering, electronic engineering, information engineering ,CubeSat ,Electrical and Electronic Engineering ,Antenna (radio) ,Aerospace engineering ,business ,Remote sensing - Abstract
This article describes the development of a deployable high-gain antenna (HGA) for the proposed Mars Cube One (MarCO) CubeSat mission to Mars. The antenna is a new folded-panel reflectarray (FPR) designed to fit on a 6U (10 ? 20 ? 34 cm3) CubeSat bus and support 8.425-GHz Mars-to-Earth telecommunications. The FPR provides a gain of 29.2 dBic with right-hand circular polarization (RHCP). Small stowage volume is a key advantage of the FPR design, as it only consumes ~4% of the usable spacecraft payload volume with a mass of less than 1 kg.
- Published
- 2017
- Full Text
- View/download PDF