Taiwan · Hapith V
TiSPACE
A hybrid-propulsion small-launch programme with published design figures
What the published evidence says
- The technology page publishes maxima of 390 kg LEO and 350 kg SSO, with a 600–700 km altitude reference.
- These are programme specifications, not independently verified current flight performance.
Current orbital flight status, programme continuity and customer mission acceptance remain unverified here.
Provider quotation and programme readiness confirmation required.
Open the original capability source ↗What still needs an answer
- Current flight readiness and a firm service date
- Mission-specific payload performance and integration
- Launch-site eligibility, export requirements and contracting terms
A design target, a suborbital demonstrator, an orbital flight and an available commercial slot are different kinds of evidence. This page does not grant compliance clearance or reserve a launch.
Put the reference in your mission context.
Start with orbit, payload mass and service preference. Confirm the open questions before making a launch decision.
Inspect the evidence
Profile reviewed 2026-10-20Published capabilities and company statements
Company publication · Reviewed 2026-10-20 · Publication date not assertedFollow subsequent announcements at the source
Company publication · Reviewed 2026-10-20 · Publication date not assertedThese are dated references. Company statements, reported tests and independent authorization are different evidence. Follow the original publication for changes.
Related company news
Spaceflight News API · original publishersTitle mentions from a limited, hourly cached search of the directory. This is news discovery, not a verified milestone feed. No result does not mean no activity; open the article to check company identity and context.
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