ᱥᱠᱟᱭᱨᱩᱴ ᱮᱨᱳᱥᱯᱮᱥ
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ᱞᱮᱠᱟᱱ | ᱯᱨᱟᱭᱵᱷᱮᱴ |
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ᱥᱤᱞᱯᱚ | ᱥᱮᱨᱢᱟᱯᱩᱨᱤ ᱵᱮᱼᱵᱮᱱᱟᱣᱤᱡ (ᱮᱨᱳᱥᱯᱮᱥ ᱥᱤᱞᱯᱚ) |
ᱦᱮᱰᱠᱩᱣᱟᱴᱚᱨ | , |
ᱢᱩᱬᱩᱛ ᱢᱟᱹᱱᱢᱤ | ᱯᱟᱣᱟᱱ ᱠᱩᱢᱟᱨ ᱪᱚᱸᱫᱽᱨᱚ (ᱜᱚᱲᱚ-ᱛᱷᱟᱯᱚᱱᱤᱡ, ᱥᱤ.ᱤ.ᱳ ᱟᱨ ᱥᱤ.ᱴᱤ.ᱳ) ᱱᱟᱜᱟ ᱵᱷᱟᱨᱚᱛᱷ ᱰᱟᱠᱟ (ᱥᱤ.ᱳ.ᱳ) |
ᱡᱤᱱᱤᱥ/ᱥᱮᱵᱟ | ᱵᱤᱠᱨᱚᱢ-ᱮᱥ ᱵᱤᱠᱨᱚᱢ-᱑ ᱵᱤᱠᱨᱚᱢ-᱒ ᱵᱤᱠᱨᱚᱢ-᱓ |
ᱥᱮᱵᱟ | ᱨᱟᱱᱟᱠᱟᱵᱽ ᱜᱟᱹᱰᱤ |
ᱟᱨᱡᱟᱣ | ᱯᱨᱤ-ᱨᱮᱵᱷᱤᱱᱤᱣ |
ᱥᱚᱦᱮᱫ |
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ᱣᱮᱵᱽᱥᱟᱭᱤᱴ | skyroot |
ᱥᱠᱟᱭᱨᱩᱴ ᱮᱨᱳᱥᱯᱮᱥ ᱯᱨᱟᱭᱵᱷᱮᱴ ᱞᱤᱢᱤᱴᱮᱰ ᱫᱚ ᱛᱮᱞᱮᱝᱜᱟᱱᱟ ᱨᱮᱭᱟᱜ ᱦᱟᱭᱫᱽᱨᱟᱵᱟᱫᱽ ᱨᱮ ᱢᱮᱱᱟᱜ ᱢᱤᱫ ᱥᱤᱧᱚᱛᱤᱭᱟᱹ ᱵᱮᱼᱥᱚᱨᱠᱟᱨᱤ ᱥᱮᱨᱢᱟᱯᱩᱨᱤ ᱵᱮᱼᱵᱮᱱᱟᱣᱤᱡ ᱟᱨ ᱵᱮᱯᱟᱨᱤᱭᱟᱹ ᱞᱚᱧᱪ ᱥᱮᱵᱟ ᱮᱢᱚᱜᱤᱡ ᱠᱟᱱᱟ᱾[᱑][᱒] ᱱᱚᱣᱟ ᱠᱚᱢᱯᱟᱱᱤ ᱫᱚ ᱤᱥᱨᱳ ᱨᱮᱱ ᱵᱟᱨᱭᱟ ᱢᱟᱨᱮ ᱥᱟᱬᱮᱥᱤᱭᱟᱹ ᱯᱟᱣᱟᱱ ᱠᱩᱢᱟᱨ ᱪᱚᱸᱫᱽᱨᱚ ᱟᱨ ᱱᱟᱜᱟ ᱵᱷᱟᱨᱚᱛᱷ ᱰᱟᱠᱟ ᱛᱟᱹᱠᱤᱱ ᱠᱤᱱ ᱵᱮᱱᱟᱣ ᱟᱠᱟᱫᱟ᱾ ᱱᱚᱣᱟ ᱨᱮᱭᱟᱜ ᱡᱚᱥ ᱫᱚ ᱛᱟᱦᱮᱸ ᱠᱟᱱᱟ ᱦᱩᱰᱤᱧ ᱥᱮᱴᱮᱞᱟᱭᱤᱴ ᱵᱟᱡᱟᱨ ᱞᱟᱹᱜᱤᱫ ᱦᱩᱰᱤᱧ ᱞᱤᱯᱷᱴ ᱞᱚᱧᱪ ᱵᱷᱮᱦᱤᱠᱮᱞ ᱩᱛᱷᱱᱟᱹᱣ ᱟᱨ ᱚᱱᱟ ᱞᱚᱧᱪ᱾
ᱱᱟᱜᱟᱢ
[ᱥᱟᱯᱲᱟᱣ | ᱯᱷᱮᱰᱟᱛ ᱥᱟᱯᱲᱟᱣ]ᱥᱠᱟᱭᱨᱩᱴ ᱮᱨᱳᱥᱯᱮᱥ ᱫᱚ ᱡᱩᱞᱟᱭ ᱒᱐᱑᱘ ᱥᱮᱨᱢᱟ ᱨᱮ ᱥᱤᱧᱚᱛᱤᱭᱟᱹ ᱥᱮᱨᱢᱟᱯᱩᱨᱤ ᱠᱷᱚᱸᱫᱽᱨᱚᱱ ᱜᱚᱱᱚᱴᱷᱚᱱ ᱨᱮᱱ ᱵᱟᱨᱭᱟ ᱥᱟᱬᱮᱥᱤᱭᱟᱹ ᱯᱟᱣᱟᱱ ᱠᱩᱢᱟᱨ ᱪᱚᱸᱫᱽᱨᱚ ᱟᱨ ᱱᱟᱜᱟ ᱵᱷᱟᱨᱚᱛᱷ ᱰᱟᱠᱟ ᱛᱟᱹᱠᱤᱱ ᱠᱤᱱ ᱵᱮᱱᱟᱣ ᱞᱮᱫᱟ᱾
ᱟᱨᱛᱷ ᱥᱴᱳᱨᱮᱵᱮᱞ ᱨᱚᱠᱮᱴ ᱤᱧᱡᱤᱱ
[ᱥᱟᱯᱲᱟᱣ | ᱯᱷᱮᱰᱟᱛ ᱥᱟᱯᱲᱟᱣ]ᱨᱟᱢᱟᱱ-᱑
[ᱥᱟᱯᱲᱟᱣ | ᱯᱷᱮᱰᱟᱛ ᱥᱟᱯᱲᱟᱣ]᱒᱐᱒᱐ ᱨᱮ, ᱥᱠᱟᱭᱨᱩᱴ ᱨᱮᱭᱟᱜ ᱧᱩᱛᱩᱢ ᱱᱮᱼᱦᱚᱲᱟᱜ ᱢᱮᱫ ᱨᱮ ᱡᱷᱟᱞᱠᱟᱣ ᱞᱮᱱᱟ, ᱡᱚᱠᱷᱚᱱ ᱱᱚᱸᱰᱮᱱᱟᱜ ᱨᱟᱢᱟᱱ-᱑ ᱦᱟᱭᱯᱟᱨᱜᱳᱞᱤᱠ-ᱯᱷᱤᱣᱮᱞ ᱟᱯᱟᱨ ᱥᱴᱮᱡᱽ ᱤᱧᱡᱤᱱ ᱮ ᱵᱤᱰᱟᱹᱣ ᱞᱮᱜᱟ ᱞᱮᱫᱟ᱾ ᱱᱚᱣᱟ ᱞᱤᱠᱩᱭᱮᱰ-ᱯᱷᱤᱣᱮᱞ ᱟᱯᱟᱨ ᱥᱴᱮᱡᱽ ᱫᱚ ᱵᱤᱠᱨᱚᱢ-᱑ ᱨᱮᱭᱟᱜ ᱦᱤᱸᱥ ᱠᱟᱱᱟ ᱟᱨ ᱥᱤᱧᱚᱛ ᱨᱮ ᱥᱠᱟᱭᱨᱩᱴ ᱨᱮ ᱯᱳᱭᱞᱳ ᱱᱚᱝᱠᱟᱱ ᱠᱟᱹᱨᱥᱤ ᱵᱮᱱᱟᱣ ᱠᱟᱛᱮ ᱮ ᱩᱫᱩᱜᱽ ᱥᱚᱫᱚᱨ ᱫᱟᱲᱮ ᱟᱠᱟᱫᱟ᱾[᱓][᱔][᱕][᱖]
ᱥᱚᱞᱤᱰ ᱨᱚᱠᱮᱴ ᱢᱳᱨᱳᱴ
[ᱥᱟᱯᱲᱟᱣ | ᱯᱷᱮᱰᱟᱛ ᱥᱟᱯᱲᱟᱣ]ᱠᱟᱞᱟᱢ-᱕
[ᱥᱟᱯᱲᱟᱣ | ᱯᱷᱮᱰᱟᱛ ᱥᱟᱯᱲᱟᱣ]ᱠᱟᱞᱟᱢ-᱑᱐0
[ᱥᱟᱯᱲᱟᱣ | ᱯᱷᱮᱰᱟᱛ ᱥᱟᱯᱲᱟᱣ]ᱠᱨᱟᱭᱳᱡᱮᱱᱤᱠ ᱨᱚᱠᱮᱴ ᱤᱧᱡᱤᱱ
[ᱥᱟᱯᱲᱟᱣ | ᱯᱷᱮᱰᱟᱛ ᱥᱟᱯᱲᱟᱣ]ᱫᱷᱟᱣᱟᱱ-᱑
[ᱥᱟᱯᱲᱟᱣ | ᱯᱷᱮᱰᱟᱛ ᱥᱟᱯᱲᱟᱣ]ᱞᱚᱧᱪ ᱵᱷᱮᱦᱤᱠᱮᱞ
[ᱥᱟᱯᱲᱟᱣ | ᱯᱷᱮᱰᱟᱛ ᱥᱟᱯᱲᱟᱣ]ᱥᱠᱟᱭᱨᱩᱴ ᱮᱨᱳᱥᱯᱮᱥ ᱟᱡᱟᱜ ᱚᱥᱟᱨ ᱜᱟᱱᱚᱜ ᱦᱤᱰᱤᱧ ᱞᱤᱯᱷᱴ ᱞᱚᱧᱪᱟᱨ ᱵᱤᱠᱨᱚᱢ ᱥᱤᱨᱤᱡᱽ Archived ᱒᱐᱒᱐-᱑᱒-᱑᱕ at the Wayback Machine. ᱨᱮᱭ ᱠᱟᱹᱢᱤ ᱠᱟᱱᱟ᱾ ᱨᱚᱠᱮᱴ ᱠᱚᱫᱚ ᱟᱹᱰᱤ ᱩᱥᱟᱹᱨᱟ ᱥᱟᱡᱟᱣ ᱠᱟᱛᱮ ᱛᱮᱭᱟᱨ ᱫᱟᱲᱮ ᱜᱟᱱᱚᱜ ᱞᱮᱠᱟ ᱵᱮᱱᱟᱣ ᱦᱩᱭᱩᱜ ᱠᱟᱱᱟ᱾[᱗] ᱱᱩᱠᱩ ᱫᱚ ᱟᱨᱦᱚᱸ ᱯᱩᱨᱟᱹᱯᱩᱨᱤ ᱫᱚᱦᱚᱲᱟ ᱛᱮ ᱵᱮᱵᱷᱟᱨ ᱜᱟᱱᱚᱜ ᱵᱷᱮᱦᱤᱠᱮᱞ (ᱨᱟᱱᱟᱠᱟᱵᱽ ᱜᱟᱹᱰᱤ) ᱪᱮᱛᱟᱱ ᱨᱮᱦᱚᱸ ᱠᱚ ᱠᱟᱹᱢᱤ ᱠᱟᱱᱟ᱾
ᱞᱚᱧᱪ ᱵᱷᱮᱦᱤᱠᱮᱞ | ᱨᱟᱱᱟᱠᱟᱵᱽ ᱫᱟᱲᱮ | ᱯᱳᱭᱞᱳ ᱩᱰᱟᱹᱱ | ᱜᱩᱴ ᱞᱚᱧᱪ | |
---|---|---|---|---|
ᱮᱥ.ᱮᱥ.ᱯᱤ.ᱳ (500 km) |
ᱞᱳ ᱟᱨᱛᱷ ᱚᱨᱵᱤᱴ (500 km; 45°) | |||
ᱵᱤᱠᱨᱚᱢ-ᱮᱥ (ᱥᱟᱵᱽᱚᱨᱵᱤᱴᱟᱨ) | - | - | ᱑᱘ ᱱᱚᱵᱜᱮᱢᱵᱚᱨ ᱒᱐᱒᱒ | ᱑ |
ᱵᱤᱠᱨᱚᱢ-᱑ | 290 kg (640 lb) | 480 kg (1,060 lb) | Q᱓ ᱒᱐᱒᱓ (ᱩᱭᱦᱟᱹᱨ ᱫᱚᱦᱚ ᱟᱠᱟᱱᱟ) | ᱐ |
ᱵᱤᱠᱨᱚᱢ-᱒ | 400 kg (880 lb) | 595 kg (1,312 lb) | TBD | ᱐ |
ᱵᱤᱠᱨᱚᱢ-᱓ | 560 kg (1,230 lb) | 815 kg (1,797 lb) | TBD | ᱐ |
ᱵᱟᱨᱦᱮ ᱡᱚᱱᱚᱲ
[ᱥᱟᱯᱲᱟᱣ | ᱯᱷᱮᱰᱟᱛ ᱥᱟᱯᱲᱟᱣ]ᱥᱟᱹᱠᱷᱭᱟᱹᱛ
[ᱥᱟᱯᱲᱟᱣ | ᱯᱷᱮᱰᱟᱛ ᱥᱟᱯᱲᱟᱣ]- ↑ Sukumar, C. R. "Skyroot India's first private company to test upper-stage rocket engine". The Economic Times. Retrieved 2020-08-12.
- ↑ Narasimhan, T. E. (2020-08-12). "Skyroot Aerospace first private company to test upper stage rocket engine". Business Standard India. Retrieved 2020-08-12.
- ↑ PTI (13 August 2020). "Hyderabad startup Skyroot Aerospace test-fires upper stage rocket engine 'Raman'". The Times of India. Archived from the original on 2022-01-09. Retrieved 2020-08-16.
- ↑ Pandey, Ashish (14 August 2020). "Hyderabad-based startup Skyroot Aerospace's Raman: India's first homegrown rocket engine". India Today (in ᱟᱝᱜᱽᱨᱮᱡᱤ). Retrieved 2020-08-16.
- ↑ Goyal, Shikha (2020-08-17). "First Indian start-up firm Skyroot Aerospace to test fire rocket engine 'Raman': All you need to know". Jagran Josh. Retrieved 2020-08-21.
- ↑ "Skyroot Aerospace becomes first Indian startup to test upper-stage rocket engine". The Asian Age. 2020-08-13. Retrieved 2020-12-14.
- ↑ "Launch Vehicle". Skyroot Aerospace. 10 January 2019. Archived from the original on 2020-12-15. Retrieved 2020-08-21.