Bilal
THINK TANK: CONSULTANT
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- #46
1. KZ-1A's motor diameter is 1.2m, Ababeel's dia is 1.4m.
2. KZ-1A has a max payload fairing diameter of 1.4m, Ababeel's fairing is much larger at 1.7-1.8m.
3. KZ-1A's payload capacity is 200kg to a 700km orbit, which is far far less than Ababeel's probable payload of >1000kg (3xMIRVs) touching ~600km apogee.
Now take your sorry tushy back to BR or wherever you go to vent out your frustration.
Actually, KZ-1A's first and second stage is 1.4m
Actually the first and second stages of the KZ-1A is 1.4m. It uses the L-SpaB-140B, although the Shaheen II series probably use a derivative of the older less powerful L-SpaB-140A motors.
You're right that KZ-1A can lift 200 kg to a SSO (Sun-Synchronous Orbit), but probably more, ~ 400 kg to a LEO,
The Ababeel could probably lift 150 - 250 kg to a LEO 600 Km orbit. I.E less powerful than the KZ-1A.
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I meant to refer to the 3rd and 4th stage where it gets much narrower (1.2m), while Ababeel remains at 1.4m throughout (except where the MIRV bus and payload fairing begin).
True about the payload capacity to orbit part, I meant to convey that the base stages and consequently 3rd stage of Ababeel is built to boost much more than 200kg. Assuming a bare minimum of 300kg per RV, that puts the total payload (including 3xRVs, MIRV-bus) to anywhere between 1000-1500kg.
Also, 3rd stage is not solid-fueled as per above sketch. Similarly the claim for same motors for KZ-1A and Ababeel/S-II/S-III is shady, its not possible that China used a 30 years old motor design in a modern day SLV.
Oh yeah. That's why I said the KZ-1A/DF-21D/DF-26 usesa new L-SpaB-140B, as oppose to the M-18/Ababeel/S-II/S-III that probably use an older gen L-SpaB-140.
'First stage motor is 1,40 meters in diameter, having a total mass of 16,621 kg, a burn time of 65 seconds and an impulse of 2,352 Ns/kg. The Second stage motor is 1,40 meters in diameter, having a total mass of 8,686 kg, a burn time of 62 seconds and an impulse of 2,810 NS/kg. The Third stage motor is 1,20 meters in diameter, having a total mass of 3,183 kg, a burn time of 55 seconds and an impulse of 2,850 NS/kg.'
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