Launch and deployment
Also known as Launch, Deployment, Rideshare, Deployer, OTV
How small satellites reach orbit: from a host satellite, directly from the launch vehicle or from an orbital transfer vehicle. For PocketQubes the launch segment has been a major cause of loss, with 13 of 77 units lost or degraded before operations.
- Document
- SQ-OP-001
- Updated
- 20 Oct 2026
- Reading time
- 5 min
In this tab
Three routes to orbit#
A small satellite reaches orbit in a deployer that something else carries. For PocketQubes three routes have been used[1]:
- From a host satellite. A microsatellite carries the deployer and releases the PocketQubes after its own separation. The first four PocketQubes left GAUSS Srl’s UniSat-5 in 2013 from the MRFOD deployer, and UniSat-7 repeated the scheme in 2021[2].
- From the launch vehicle. The deployer rides on the rocket itself, as AlbaPods did on Rocket Lab’s Electron in 2019 and on SpaceX’s Transporter rideshares.
- From an orbital transfer vehicle (). A free-flying carrier such as D-Orbit’s ION, or once Launcher’s Orbiter, separates from the rocket and releases its passengers later, possibly into different orbits.
The balance has shifted towards transfer vehicles: from 2022 onwards they became the dominant route and carried all 20 PocketQubes launched in 2023[3].
Deployers#
| Deployer | Developer | Notes |
|---|---|---|
| MRFOD | Morehead State University and GAUSS | Morehead–Rome FemtoSat Orbital Deployer, flown inside UniSat-5 |
| AlbaPod | Alba Orbital | AlbaPod v2 carries up to six units, weighs less than 500 g and was specified for at least 2 m/s ejection; by 2024 it had flown eight missions and deployed 41 PocketQubes |
| PicoBus | Libre Space Foundation | Open-hardware PocketQube deployer, flown on both Firefly Alpha missions[4] |
The v2 shell, ejection mechanism and door are laser-sintered from the carbon-filled polyamide Windform XT 2.0, which cut its mass by about 60% compared with its predecessor[5].
References
- [1]nadir lab. (2026). PocketQube picosatellites: A review of standards, mission trends and miniaturization constraints, with lessons learned from Grizu-263A, Türkiye’s first PocketQube [Preprint]. nadir lab.Read on nadir lab.
- [2]Krebs, G. D. (2026). UniSat 5. Gunter’s Space Page.space.skyrocket.de(accessed 20 October 2026)
- [3]Krebs, G. D. (2026). PocketQube (PocketQub). Gunter’s Space Page.space.skyrocket.de(accessed 20 October 2026)
- [4]Libre Space Foundation. (2026). LSF-PICOBUS PocketQube deployer.libre.space(accessed 20 October 2026)
- [5]nadir lab. (2026). Materials engineering for PocketQube picosatellites: A scaling-based review and design guide [Preprint]. nadir lab.Read on nadir lab.
- [6]Wall, M. (2022). Firefly Aerospace’s Alpha rocket reaches orbit for 1st time. Space.com.space.com(accessed 20 October 2026)
- [7]SpaceNews. (2022). Report on the outcome of Firefly Alpha flight FLTA002.spacenews.com(accessed 20 October 2026)
- [8]Bouwmeester, J., Radu, S., Uludag, M. S., Chronas, N., Speretta, S., Menicucci, A., & Gill, E. K. A. (2020). Utility and constraints of PocketQubes. CEAS Space Journal, 12(4), 573–586.doi:10.1007/s12567-020-00300-0
- [9]The CubeSat Program, Cal Poly SLO. (2022). CubeSat Design Specification, Rev. 14.1 (CP-CDS-R14.1). California Polytechnic State University.nasa.gov
- [10]Alba Orbital, TU Delft, & GAUSS Srl. (2018). The PocketQube Standard, Issue 1.albaorbital.com
- [11]Uludag, M. S., Yakut, E., Speretta, S., Radu, S., Chronas-Foteinakis, N., Bouwmeester, J., Menicucci, A., & Gill, E. (2019). Getting the Delfi-PQ ready for multiple launch options. In: International Symposium on Space Technology and Science (ISTS), Fukui (2019-f-08).pure.tudelft.nl
- [12]Libre Space Foundation community forum. (2022). SpaceX F9 Transporter-3, 2022-01-13 15:25 UTC (discussion thread).community.libre.space(accessed 20 October 2026)
Cite this SatWiki entry
@misc{nadirlab2026launch,
author = {{nadir lab.}},
title = {{Launch and deployment}},
year = {2026},
month = oct,
howpublished = {nadir lab. SatWiki SQ-OP-001 (Rev. 1)},
url = {https://nadirlab.space/en/wiki/launch-deployment/}
}nadir lab. (2026). Launch and deployment. nadir lab. SatWiki (SQ-OP-001, Rev. 1). https://nadirlab.space/en/wiki/launch-deployment/
TY - ENCYC
AU - {nadir lab.}
TI - Launch and deployment
T2 - nadir lab. SatWiki
PY - 2026
ET - Rev. 1
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