nuclear thermal rocket
form of rocket propulsion
Facts
3 properties- Subclass of
- nuclear propulsion, rocket engine
- Defining formula
- \Delta v\ = V_e \ln \frac {m_0} {m_1}
- Maintained by WikiProject
- WikiProject Mathematics[3]
🏷️ Also known as
en NTR
en nuclear thermal rocket
ar صاروخ نووي حراري
de Nukleares Raketentriebwerk
es Propulsión termonuclear
es Propulsion termonuclear
fa راکت حرارتی هستهای
fi ydinlämpöraketti
fr propulsion nucléaire thermique
id Roket termal nuklir
it Razzo termico nucleare
ja 核熱ロケット
ko 핵추진로켓
ko 핵열 로켓
pl Silnik nuklearny
pt Foguete termonuclear
ru атомный ракетный двигатель
ru ядерный двигатель
ru ядерный ракетный двигатель
ru ядерный реактивный двигатель
🔖 Identifiers · 9
- Library of Congress Authorities ID
- sh85093102
- BNCF Thesaurus ID
- 30470
- Bibliothèque nationale de France ID
- 119777556
- Freebase ID
- /m/09fnm
- Great Russian Encyclopedia Online ID (2017)
- 4924254
- J9U entity ID
- 987007538644205171
- Microsoft Academic ID (discontinued)
- 2778447519
- Quora topic ID
- Nuclear-Thermal-Rocket
- Yale LUX ID
- concept/bf0e0bb4-800d-4fe4-b235-23270bb7b1f5
🔗 Connections
Subclass of 2
Maintained by WikiProject 1
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