HARDWARE / PRODUCTUpdated 8 Aug 2026

Promin 1 (Zaarbird)

Promin Aerospace
Promin 1 (Zaarbird)

Ultra-light autophagic small-satellite launch vehicle carrying pico/nanosatellite payloads to orbit.

Key figurescomparable across the catalogue

Mass
100 kg

Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.

As published by the supplier

Vehicle mass (approx.)
~100 kg
Payload class
Pico/nanosatellites, target ~0.1-3 kg to LEO (launcher family spans 100-500 kg mass class)
Propulsion technology
Autophagic (self-devouring) solid-fuel engine; fuel tank doubles as airframe, gasified and burned in flight with pulsation combustion
Orbital debris
Designed to leave no spent stage/tank structure in orbit
Turnaround time
As little as ~1 month from order to launch (company target)
Target launch price
~$150,000-$200,000 per launch (early public estimate)
Development status
Ground engine/fuel testing since 2021; suborbital test campaign planned from Brunswick, Maine, US

About

Promin 1 (also referred to by the internal name Zaarbird) is Promin Aerospace’s ultra-light orbital launch vehicle built around the company’s proprietary autophagic propulsion technology. Instead of carrying a separate metal or composite fuel tank, the rocket’s solid-fuel propellant grain doubles as the vehicle’s own structural airframe: as the engine burns, it progressively gasifies and consumes the fuel-tank material itself in a pulsation-combustion process, shedding structural mass in flight the way a candle burns down. This ‘self-devouring’ design sharply reduces passive (dead) mass and mitigates the scale-factor penalty that normally makes very small launch vehicles inefficient, allowing Promin 1 to be one of the lightest orbital-class rockets in the world at roughly 100 kg gross liftoff mass.

The vehicle is sized for the pico- and nanosatellite segment, targeting delivery of payloads on the order of a few kilograms to orbit (early public figures cite roughly 0.1-3 kg to LEO, with the company’s broader launcher family spanning a 100-500 kg mass class). Because most of the airframe is consumed during ascent, the design is intended to leave little to no spent-stage debris in orbit, addressing a longstanding sustainability concern for the smallsat launch market. Promin Aerospace states that turnaround from order to launch can be as short as about one month, aimed at underserved customers — research groups, universities, and organizations in countries without national launch capability — who need dedicated, responsive access to orbit rather than waiting for rideshare slots.

Development has proceeded through autophagic engine and solid-fuel combustion ground testing conducted in Ukraine beginning in 2021, including a notable large-scale fuel-combustion test in December 2021 and continued engine test campaigns through 2022 despite the full-scale Russian invasion. The programme has publicly targeted a progression from short-hop/suborbital test flights toward an orbital demonstration, with the company also pursuing launch-site agreements (memoranda of understanding with the Atlantic Spaceport Consortium in the Azores and Spaceport 1 in Scotland) and, more recently, a US-based flight-test campaign from Brunswick, Maine, supported by Promin Aerospace’s US office opened in December 2024.

Documentation

No public datasheet yet — request the datasheet / ICD from the supplier.

Source: prominaerospace.com ↗

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