Aerospace System Design¶
NASA-hosted original. Aerospace System Design: Mission Analysis.
Cited by¶
1 citation across 1 artifact.
Each citation links to the sentence it supports in the citing article.
Domain-specific¶
- Gravity Loss
- The comparison requires a stated target and model: the same gravitational acceleration can hinder an ascent, aid a passive descent, or require upward thrust to hold a lander at a controlled descent rate.
This source(7.4), constant-rate lunar descent; the indexed passage was inspectable, but full PDF viewer access was limited in this review and should be rechecked before production reference binding.
- The comparison requires a stated target and model: the same gravitational acceleration can hinder an ascent, aid a passive descent, or require upward thrust to hold a lander at a controlled descent rate.
Verification¶
Does it exist? Not checked yet. This entry carries no identifier to resolve. It was extracted from the citation as written in the article, normalized, and deduplicated against the rest of the registry.
Does it back the claim? Not recorded. The single citation of this work carries no recorded support check.
Support is checked per citation rather than per work — the same source can be cited soundly in one article and wrongly in another. Per-citation recording began recently, so a citation with no recorded check is a gap in the record rather than evidence it went unchecked.
See how references were verified.
Registry ID ref:b291ec0fed30 · see in the full table