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>> No.11988416 [View]
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11988416

>During development, Glushko studied the use of pentaborane "zip" propellants in a modified RD-270M engine. This would have created immense toxicity problems but increased the specific impulse of the engine by 42 seconds (0.41 km/s).[4]

>> No.11821557 [View]
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11821557

>The first test flight occurred on December 16, 1965.[20] It missed the landing area by a wide margin owing to a stabilization instrument malfunction. The second test was on February 5, 1966 and was also a failure due to a retrorocket issue.[20] The third test took place on March 16, 1966.[20] Nitrogen tetroxide spilled over the surface pad during fueling due to a miscommunication and the missile was quickly destroyed by fire. Some success was had with the fourth test on May 20, 1966, but the payload didn't break away from the missile's guidance system as intended.[20] The following tests were conducted from silos.[20] The first two tests of the silo phase ended in the intentional destruction (via self-destruct functionality) of the R-36O as a result of the second stage engine accidentally being activated for too long, sending the payload into an unplanned orbit. NATO radar systems picked up on the large mass of resulting debris.[20][21] In one failed test case, small pieces of the missile rained down on the midwestern United States.[21]

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