With the new added third stage. We can now all be confident that the Ababeel missile is the basic configuration for Pakistan's SLV. It can probably lift a payload of around 150 - 250 kg (maybe 290?) into LEO covering about 250 - 500 Km. A small hydrazine fueled fourth stage could be added like China's KZ-1.
Personally I'm a little disappointed they couldn't acquire the technology for a larger diameter motor, of maybe 1.70 m, but beggars can't be choosers.
I expect a full SLV test will be conducted with a dummy satellite within the next year. What are the implications for Pakistan?
Personally I'm a little disappointed they couldn't acquire the technology for a larger diameter motor, of maybe 1.70 m, but beggars can't be choosers.
I expect a full SLV test will be conducted with a dummy satellite within the next year. What are the implications for Pakistan?
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