Antennas & deployment mechanisms
Also known as Tape-spring antenna, Burn wire, UHF dipole
Quarter-wave and half-wave UHF tape-spring antennas, S-band patch arrays, UHMWPE thermal-knife hold-downs and deployment verification switches on picosatellites.
- Document
- SQ-SS-009
- Updated
- Reading time
- 1 min
In this tab
Why UHF antennas must deploy on a 5 cm cube
At the amateur UHF satellite band (, wavelength ), a quarter-wave monopole measures and a half-wave dipole —three to seven times the edge of a PocketQube[1]. An electrically small antenna kept flush with a face () suffers a low radiation resistance and high reactive near field, losing of efficiency relative to a deployed wire[2]. Consequently, almost every UHF PocketQube stows flexible spring-steel or beryllium–copper (CuBe2) tape elements wrapped around the chassis during launch and releases them after separation[3].
Thermal-knife (burn-wire) hold-downs
Pyrotechnic cutters are prohibited on CubeSats and PocketQubes[4]. Instead, the coiled antenna tape is tied down with a braided ultra-high-molecular-weight polyethylene (UHMWPE, Dyneema, melting point ) or Vectran cord pressed against a surface-mount nichrome (NiCr) resistor or spring-loaded heating element[3]:
- Redundant inhibit chain: Two mechanical deployment switches on the keep the spacecraft unpowered inside the deployer. After ejection, the flight software waits at least before arming the burn circuit.
- Constant-power burn pulse: Driving through a surface-mount resistor or NiCr wire severs a UHMWPE line in in vacuum. A spring-loaded rocker or tensioned loop ensures constant contact force as the polymer softens.
- Ground plane and balun: Because a chassis is less than across at , a single monopole uses the hull itself as a counterpoise, tilting the radiation pattern; symmetric dipoles fed via a miniature lumped-element balun avoid chassis-current detuning[1].
References
- [1]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).Read on nadir lab.
- [2]NASA Small Spacecraft Systems Virtual Institute. (2026). Communications. State-of-the-Art of Small Spacecraft Technology (2026 edition), Chapter 9. NASA Ames Research Center.nasa.gov(accessed 20 October 2026)
- [3]nadir lab. (2026). A review of structural, thermal, magnetic and electronic materials in PocketQube-class picosatellites [Preprint]. nadir lab. Research Monographs (SQ-R-002).Read on nadir lab.
- [4]Alba Orbital, TU Delft, & GAUSS Srl. (2018). The PocketQube Standard, Issue 1.albaorbital.com
Cite this SatWiki entry
@misc{nadirlab2026antennas,
author = {{nadir lab.}},
title = {{Antennas \& deployment mechanisms}},
year = {2026},
month = oct,
howpublished = {nadir lab. SatWiki SQ-SS-009 (Rev. 1)},
url = {https://nadirlab.space/wiki/antennas-deployment/}
}nadir lab. (2026). Antennas & deployment mechanisms. nadir lab. SatWiki (SQ-SS-009, Rev. 1). https://nadirlab.space/wiki/antennas-deployment/
TY - ENCYC AU - nadir lab. TI - Antennas & deployment mechanisms T2 - nadir lab. SatWiki PY - 2026 ET - Rev. 1 C1 - SQ-SS-009 UR - https://nadirlab.space/wiki/antennas-deployment/ ER -