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instrument implementation / implementation-contract
Rocket Equation (Tsiolkovsky) implementation
A source-bound implementation contract for Rocket Equation (Tsiolkovsky); deployment and executable qualification remain separate.
Binding contract
This record describes what an executable surface must bind and validate. It does not claim that a public calculator, package, or production route is deployed.
- Record owner
- Guth Instruments
- Lifecycle
- verified-with-binding-errata
- Evidence ID
- t4-233
- Effect
- Computation or source lookup only
Input and validation requirements
The zero-final-mass input creates a division-by-zero and undefined logarithm argument; the instrument must reject it rather than return a finite value. Directional and input-representation conventions can also produce sign or interpretation errors if not explicitly labeled.
Required corrections
[
{
"vector": 3,
"field": "required_propellant_kg",
"wrong": 3202.32,
"correct": 3202.46,
"cause": "exp(3000/3138.128) hand-evaluated slightly low"
}
]Inspectable interface fixture
The sample below is evidence for interface and validation tests, not a production implementation.
{
"inputs": {
"Isp_s": 300,
"m0_kg": 10000,
"mf_kg": 4000,
"g0_m_per_s2": 9.80665
},
"expected_outputs": {
"delta_v_m_per_s": 2695.7228
},
"working": "ve = Isp·g0 = 300·9.80665 = 2941.995 m/s. Mass ratio = m0/mf = 10000/4000 = 2.5. ln(2.5) = 0.916290732. Delta-v = 2941.995·0.916290732 = 2695.7228 m/s."
}Other records
Sources and evidence
These pointers bind the page to evidence. They do not grant authority or collapse verification into deployment.
VERIFIED_LEDGER.jsonevidence-tranche4/tranche4-results.jsontranche errata record