Launch Vehicle Cost Allocation Overruns
Definition
In launch vehicle cost allocation, inert mass fraction drives up costs; optimization shows minimum costs at specific payload sizes, but errors lead to overruns in production and operations.[1][3]
Key Findings
- Financial Impact: AUD 13-20M per fly-away launch; 65% contractor costs overrun due to non-optimized allocation.[3]
- Frequency: Per launch mission
- Root Cause: Suboptimal flights per vehicle (Nfpv) and payload mass (MpL) selection in costing models.
Why This Matters
The Pitch: Space research firms in Australia 🇦🇺 face AUD 20M+ fly-away costs per launch due to poor cost allocation. Automation of parametric optimization eliminates excess inert mass costs.
Affected Stakeholders
Cost Engineers, Program Managers, Launch Contractors
Deep Analysis (Premium)
Financial Impact
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Current Workarounds
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Methodology & Sources
Data collected via OSINT from regulatory filings, industry audits, and verified case studies.
Related Business Risks
Suboptimal Launch Cost Decisions
Launch Operations Cost Inflation
Estimation Method Inaccuracies
Flight Hardware Inventory Chain Overheads
Equipment Idle in Payload Qualification
Inventory Shrinkage in Space Supply Chains
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