Source-supported parameter
0A supported parameter does not qualify the whole vehicle or container.
ORBITAL / STATUS UNVERIFIED
Eris
Gilmour Space · Australia
Capacity: operator confirmation required
Explore technical data · Launch opportunities · Calculate my cargoErisConfiguration record — no approved dimensional illustration
Technical overview
This family record requires variant documentation. Performance, geometry, interfaces and environment must be reviewed for the specific configuration and mission.
- Eris
Technical specifications
Browse by category. Each value applies to the configuration described in its conditions; review date is not document date.
Historical / reference data
3Applies to a stated period or variant.
Engineering review required
0Do not use as an approved design constraint.
Dimensions and mass
| Parameter | Value and applicability | Confidence and source |
|---|---|---|
| Test vehicle length | 23 m; Test Flight 1 | Historical / reference data Reviewed: 2026-10-13 |
Stages, propulsion and structure
| Parameter | Value and applicability | Confidence and source |
|---|---|---|
| Test vehicle stages | 3 | Historical / reference data Reviewed: 2026-10-13 |
History and configuration context
| Parameter | Value and applicability | Confidence and source |
|---|---|---|
| Test flight location | Bowen Orbital Spaceport, Abbot Point, North Queensland | Historical / reference data Reviewed: 2026-10-13 |
Payload performance
No approved performance set with complete orbital conditions. Published lift capability is not available capacity.
LEO
NOT PUBLICLY VERIFIED
SSO
NOT PUBLICLY VERIFIED
POLAR
NOT PUBLICLY VERIFIED
MEO
NOT PUBLICLY VERIFIED
GTO
NOT PUBLICLY VERIFIED
GEO
NOT PUBLICLY VERIFIED
HEO
NOT PUBLICLY VERIFIED
LUNAR TRANSFER
NOT PUBLICLY VERIFIED
DEEP SPACE
NOT PUBLICLY VERIFIED
Fairing & payload geometry
Eris — NOT_PUBLICLY_VERIFIED
External diameter: NOT PUBLICLY VERIFIED
INSUFFICIENT_GEOMETRY_DATA · NOT_PUBLICLY_VERIFIED · NOT VERIFIED
Adapters: NOT PUBLICLY VERIFIED
Fairing diameter is not usable diameter. A digitized static profile does not confirm dynamic clearance or flight qualification.
Open existing geometry engineLaunch environment
Vibration, acoustics, quasi-static loads, shock, venting, thermal conditions and contamination require variant-specific profiles.
ENGINEERING VERIFICATION REQUIRED
Launch services
Dedicated service, rideshare, separation or orbital transfer requires operator and mission confirmation. HASTE is suborbital and is not an orbital launch offer.
Launch history
A complete verified history has not been imported. Reliability is not calculated from a partial catalog.
Historical launch cost & price intelligence
PRICE ON REQUEST · Price and terms require renewed verification
ILS launch opportunities
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Full catalog and capacity confirmationsSLX BOX — REV 2.0
SLX BOX MICRO
380 × 380 × 560 mm
Designed interior: 350 × 350 × 520 mm
ENGINEERING VERIFICATION REQUIRED
SLX BOX STANDARD
850 × 850 × 1240 mm
Designed interior: 810 × 810 × 1180 mm
ENGINEERING VERIFICATION REQUIRED
SLX BOX HEAVY
1840 × 1840 × 2700 mm
Designed interior: 1760 × 1760 × 2600 mm
ENGINEERING VERIFICATION REQUIRED
Tare mass, stacking, mounts and flight qualification remain unverified.
Preliminary calculator
INDIVIDUAL QUOTATION REQUIRED
Unknown hardware mass prevents a complete quote. Dimensions do not establish container qualification.
Continue — ISO, temperature, ESD and inquiryPDF documentation
Download technical datasheet PDFThe technical datasheet is separate from the private cargo estimate generated after saving an inquiry.
REFERENCE / ENGINEERING REVIEW · 2026-11-10
Source documentation
Verification of one parameter does not verify the whole page. Space LogistiX does not claim operator partnership or qualification.