CanSat
Auch bekannt als CanSat, ARLISS
Ausbildungsplattform im Getränkedosenformat für Atmosphärenabstiege und Systemtechnik-Training.
- Dokument
- SQ-FF-006
- Aktualisiert
- Lesezeit
- 2 min
In diesem Reiter
Definition and educational role
A CanSat is a non-orbital satellite simulator integrated inside the volume of a standard beverage can ( diameter by height, , mass )[1]. Unlike a PocketQube or CubeSat, a CanSat never reaches orbital velocity: it is lofted to by a small sounding rocket, captive balloon or multi-rotor drone, ejected at apogee and recovered under a parachute while transmitting live telemetry to a portable ground station[2].
Robert J. Twiggs proposed the concept in 1998 at the University Space Systems Symposium (USSS) in Hawaii, and the first ARLISS (A Rocket Launch for International Student Satellites) flights took place at Black Rock Desert, Nevada, in September 1999[1]. That hands-on progression led directly to the CubeSat standard (1999) and later the PocketQube standard (2009)[3].
Subsystems shared with a 1P PocketQube
Although a CanSat operates in convective air rather than high vacuum and free-molecular flow, four subsystem disciplines carry over directly to a PocketQube project[3]:
- Power bus and umbilical inhibit: A single Li-ion or LiPo cell, a mechanical remove-before-flight () pull pin and current telemetry mirror the inhibit architecture of an orbital EPS.
- Packet radio and link margin: UHF/ISM transceivers ( or , or ) require the same framing, CRC validation and ground-station Yagi tracking used during commissioning.
- Shock and deployment loads: Ejection from a rocket fairing at and parachute snatch force expose solder joints, connectors and battery mounts to mechanical transients comparable to launch vibration[2].
- What changes in orbit: Moving from a CanSat to a PocketQube removes convective cooling, introduces thermal and battery eclipse cycles per year, requires low- materials () and increases link range from to .
Literaturverzeichnis
- [1]Twiggs, R. J. (2009). Making it small: the PocketQub. CubeSat Developers’ Workshop, San Luis Obispo (archived presentation).web.archive.org(abgerufen am 20. Oktober 2026)
- [2]NASA CubeSat Launch Initiative. (2017). CubeSat 101: Basic Concepts and Processes for First-Time CubeSat Developers. NASA.nasa.gov(abgerufen am 20. Oktober 2026)
- [3]nadir lab. (2026). PocketQube-class picosatellites: architecture, flight heritage, and a multi-method post-flight analysis of Grizu-263A [Preprint]. nadir lab. Research Monographs (SQ-R-001).Auf nadir lab. lesen
Diesen SatWiki-Eintrag zitieren
@misc{nadirlab2026cansat,
author = {{nadir lab.}},
title = {{CanSat}},
year = {2026},
month = oct,
howpublished = {nadir lab. SatWiki SQ-FF-006 (Rev. 1)},
url = {https://nadirlab.space/de/wiki/cansat/}
}nadir lab. (2026). CanSat. nadir lab. SatWiki (SQ-FF-006, Rev. 1). https://nadirlab.space/de/wiki/cansat/
TY - ENCYC AU - nadir lab. TI - CanSat T2 - nadir lab. SatWiki PY - 2026 ET - Rev. 1 C1 - SQ-FF-006 UR - https://nadirlab.space/de/wiki/cansat/ ER -