CubeSat Standards Handbook 2025

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This is by far the most important thing to have. Then, in no particular order: One or more radios: plus antennas, encoders/decoders, etc. Power: solar cells, batteries GNC (Guidance, navigation, control): a flight computer, gyroscopes, star tracker, accelerometers Propulsion: thrusters, magnetic torquers.
Structural Requirements The CubeSat structure must be compatible with the P-POD. Rails must be smooth and edges must be rounded to a minimum radius of 1 mm. At least 75% (85.125 mm of a possible 113.5mm) of the rail must be in contact with the P-POD rails.
The CubeSat rails and envelope shall adhere to the dimensional specification outlined in Figure 4.1. 1-1. Each CubeSat rail shall have a minimum width (X and Y faces) of 6mm. The edges of the CubeSat rails shall have a radius of 0.5mm +/- 0.1mm.
CubeSats are a class of nanosatellites that use a standard size and form factor. The standard CubeSat size uses a one unit or 1U measuring 10x10x10 cms and is extendable to larger sizes; 1.5, 2, 3, 6, and even 12U.
Cubesat Space Protocol (CSP) is a small protocol stack written in C. CSP is designed to ease communication between distributed embedded systems in smaller networks, such as Cubesats. The design follows the TCP/IP model and includes a transport protocol, a routing protocol and several MAC-layer interfaces.
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The CubeSat standard structures, also referred to as canisterized satellites, include 1U, 1.5U, 2U, 3U, 6U, and 12U. Larger sizes exists but are less common. Table 6-1 shows the nominal weight limits and dimensions of each CubeSat structure from the CubeSat Design Specification document.
Modal analysis is a structural analysis conducted on CubeSats to validate the structural integrity of the models connections and calculate natural frequencies, particularly the fundamental frequency. It determines the mode shapes and vibration patterns.

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