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Small Satellite Launch Rocket "ZERO"

Supported the development of CFRP for key components, such as the satellite fairing, contributing to weight reduction and quality assurance.

"ZERO" is a liquid-fuel rocket currently under development by Interstellar Technologies, Inc., and provides a dedicated space transportation service for small satellites. Our company has been involved in the development process since the prototype stage, using CFRP for key components such as the satellite fairing, satellite payload, and fuselage. We developed a parts manufacturing process based on analysis, contributing to weight reduction. We also maximized our in-house facilities, contributing to quality assurance.

Client Interstellar Technologies, Inc.
URL https://www.istellartech.com/en
Application Small satellite launch vehicle
Development Part Satellite fairing / Satellite payload / Fuselage
Required Characteristics Lightweight / Rigidity / Impact resistance
Development Scope Design / Structural analysis / Evaluation testing / Prototyping / Manufacturing
Development Period Approximately 3 years (ongoing)
Molding Method Autoclave
Size Aircraft specifications : Length 32m, Diameter 2.3m
Weight Aircraft specifications : 71t

Development Case Studies