Faster access than browser!Similarities between LGM-25C Titan II and LR-87
LGM-25C Titan II and LR-87 have 13 things in common (in Unionpedia): Aerojet, Aerozine 50, Dinitrogen tetroxide, HGM-25A Titan I, Hydrazine, Hypergolic propellant, Intercontinental ballistic missile, Liquid-propellant rocket, LR91, NASA, Project Gemini, Titan (rocket family), Unsymmetrical dimethylhydrazine.
Aerojet
Aerojet was an American rocket and missile propulsion manufacturer based primarily in Rancho Cordova, California, with divisions in Redmond, Washington, Orange and Gainesville in Virginia, and Camden, Arkansas.
Aerojet and LGM-25C Titan II · Aerojet and LR-87 ·
Aerozine 50
Aerozine 50 is a 50/50 mix by weight of hydrazine and unsymmetrical dimethylhydrazine (UDMH), originally developed in the late 1950s by Aerojet General Corporation as a storable, high-energy, hypergolic fuel for the Titan II ICBM rocket engines.
Aerozine 50 and LGM-25C Titan II · Aerozine 50 and LR-87 ·
Dinitrogen tetroxide
Dinitrogen tetroxide, commonly referred to as nitrogen tetroxide, is the chemical compound N2O4.
Dinitrogen tetroxide and LGM-25C Titan II · Dinitrogen tetroxide and LR-87 ·
HGM-25A Titan I
The Martin Marietta SM-68A/HGM-25A Titan I was the United States' first multistage intercontinental ballistic missile (ICBM), in use from 1959 until 1965.
HGM-25A Titan I and LGM-25C Titan II · HGM-25A Titan I and LR-87 ·
Hydrazine
Hydrazine is an inorganic compound with the chemical formula (also written), called diamidogen, archaically.
Hydrazine and LGM-25C Titan II · Hydrazine and LR-87 ·
Hypergolic propellant
A hypergolic propellant combination used in a rocket engine is one whose components spontaneously ignite when they come into contact with each other.
Hypergolic propellant and LGM-25C Titan II · Hypergolic propellant and LR-87 ·
Intercontinental ballistic missile
An intercontinental ballistic missile (ICBM) is a guided ballistic missile with a minimum range of primarily designed for nuclear weapons delivery (delivering one or more thermonuclear warheads).
Intercontinental ballistic missile and LGM-25C Titan II · Intercontinental ballistic missile and LR-87 ·
Liquid-propellant rocket
A liquid-propellant rocket or liquid rocket is a rocket engine that uses liquid propellants.
LGM-25C Titan II and Liquid-propellant rocket · LR-87 and Liquid-propellant rocket ·
LR91
The LR91 was an American liquid-propellant rocket engine, which was used on the second stages of Titan intercontinental ballistic missiles and launch vehicles.
LGM-25C Titan II and LR91 · LR-87 and LR91 ·
NASA
The National Aeronautics and Space Administration (NASA) is an independent agency of the executive branch of the United States federal government responsible for the civilian space program, as well as aeronautics and aerospace research.
LGM-25C Titan II and NASA · LR-87 and NASA ·
Project Gemini
Project Gemini was NASA's second human spaceflight program.
LGM-25C Titan II and Project Gemini · LR-87 and Project Gemini ·
Titan (rocket family)
Titan is a family of United States expendable rockets used between 1959 and 2005.
LGM-25C Titan II and Titan (rocket family) · LR-87 and Titan (rocket family) ·
Unsymmetrical dimethylhydrazine
Unsymmetrical dimethylhydrazine (UDMH; 1,1-dimethylhydrazine) is a chemical compound with the formula H2NN(CH3)2.
LGM-25C Titan II and Unsymmetrical dimethylhydrazine · LR-87 and Unsymmetrical dimethylhydrazine ·
The list above answers the following questions
- What LGM-25C Titan II and LR-87 have in common
- What are the similarities between LGM-25C Titan II and LR-87
LGM-25C Titan II and LR-87 Comparison
LGM-25C Titan II has 104 relations, while LR-87 has 33. As they have in common 13, the Jaccard index is 9.49% = 13 / (104 + 33).
References
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