Journal of Thermal Engineering
metadata only
Radiation Heat Transfer in the Fuel of Nuclear Rocket
Nuclear power propulsion for space applications is essential for long term high payload missions. Several nuclear reactor types were investigated between the late 1950’s and early 1970’s under the National Aeronautical and Space Administration’s (NASA) Nuclear Engine for Rocket Vehicle Application (
Conceptio Open Archive
Analyze & explore related research in Conceptio
Connect this record directly into your research workflow or AI agent. Explore citations across open repositories, query full text, and export structured proof bundles.
This document is indexed with metadata only: full text is not available in the archive for this record. Open the official source ↗
Related documents
- The 68Ge/68Ga generator for enhancing productivity and reducing costs in nuclear medicine: experience from a university hospital#284304
- 42 U.S.C. § 13494 — Prototype demonstration of advanced nuclear reactor technology#589603
- 42 U.S.C. § 18385 — On-going restoration of radioisotope thermoelectric generator material production#588508
- Safety of Nuclear Reactor#70618
- Design and Analysis of an Alkaline Fuel Cell#940247
Record · ID 932308
Retrieved via Conceptio: every document is proof-bundled with source, license, and retrieval metadata.
Retrieved via Conceptio: every document is proof-bundled with source, license, and retrieval metadata.
Bring this data into your agent: Connect via MCP or API · 20 free credits to start · no card required
Read the Docs → · View CLI source on GitHub · Conceptio Open Knowledge Archive
Read the Docs → · View CLI source on GitHub · Conceptio Open Knowledge Archive