ຍານພາຫະນະຍິງແບບລວມ ແລະ ລະບົບດາວທຽມ
This Laos Patent “A COMBINED LAUNCH VEHICLE AND SATELLITE SYSTEM” is a public DIP intellectual-property record, filed by AGNIKUL COSMOS PRIVATE LIMITED on 2021-12-15; current status: Awaiting formal examination. Identifiers include application No. P/902; DIP id LAP902; protection kind Patent - PCT National Phase. Key dates: publication 2026-04-24. Classification: B64G 1/00、B64G 1/40、B64G 1/64. Inventor(s)/designer(s): RAVICHANDRAN, Srinath, SHAH KHADRI, Syed Peer Mohamed. Abstract hint: The present invention relates to a combined launch vehicle and satellite system. More specifically relates to the satellite combined with t…. Status labels may change after office actions; refresh or consult primary DIP data before commercial decisions.
P/902
Mark
Key facts
- Type
- Patent
- App. no.
P/902- Status
- Awaiting formal examination
- Applicant
- AGNIKUL COSMOS PRIVATE LIMITED
- Agent
- ACTIP (LAO) IP CO., LTD.
- Filing date
- 2021-12-15
- Publication
- 2026-04-24
- Protection kind
- Patent - PCT National Phase
- Priority
- IN · 202041054598 · 2020-12-15
- Applicant address
- AGNIKUL COSMOS PRIVATE LIMITED · 910, Syndicate Bank Colony, Anna Nagar West Extension, Chennai, Tamil Nadu 600101, India · IN
- Agent address
- ACTIP (LAO) IP CO., LTD. · Sisavath Village, Chanthabouly District, Vientiane, Lao PDR · LA
- Nice / IPC classes
- B64G 1/00 · B64G 1/40 · B64G 1/64
- Goods / services
- —
Process
Steps follow the current public status-
Filed
-
Formal examination In progress
-
Substantive examination
-
Published
-
Granted
Related records
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Abstract
ສິງປະດິດໃນປະຈຸບັນກ່ຽວຂ້ອງກັບຍານປ່ອຍຈະຫຼວດແບບລວມ ແລະ ລະບົບດາວທຽມ. ກ່ຽວຂ້ອງໂດຍສະເພາະກ່ຽວຂ້ອງກັບດາວທຽມທີ່ລວມກັບສ່ວນເທິງຂອງຍານປ່ອຍຈະຫຼວດເພື່ອໃຫ້ລະບົບທີ່ມີປະສິດທິພາບຫຼາຍຂື້ນ ຊຶ່ງລວມເຖິງເຕັກໂນໂລຊີການແຍກຖັງຊຶ່ງຊ່ວຍເຮັດໃຫ້ໄດ້ໂດຍໃຊ້ແຖບເມີແມນ ຫຼື ລະບົບແຍກແບບນິວເມຕິກ ໂດຍຖັງດ້ານລຸ່ມ 3 ຖັງ (105) ຈະຖືກເທອອກກ່ອນ (202) ໃນລະຫ່ວາງຂະບວນການຕາມດ້ວຍການແຍກຊຸດຖັງເປົ່າເຫຼົ່ານິ້ (203) ໃນທີ່ນີ້ເຊື້ອໄຟຈະຖືກເຕີມຈົນໝົດໃນຖັງຊຸດທີສອງ (203). ຖັງຊຸດທໍາອິດ (103) ຈາກນັ້ນຈະຖືກແຍກອອກຈາກກັນຫຼັງຈາກນັ້ນມັນເຊື້ອໄຟໝົດ (204). ໃນທໍານອງດຽວກັນ, ທໍ່ນໍ້າ (106) ຍັງຖືກແຍກອອກຈາກກັນພ້ອມກັບ ເມື່ອແຍກຖັງ. ການແຍກສ່ວນປະກອບທີ່ໃຊ້ແລ້ວໄດ້ເຮັດສໍາເລັດໃນທີນີ້ (205) ແລະ ດາວທຽມກໍພ້ອມສໍາລັບການແຊກວົງໂຄຈອນ(206).
The present invention relates to a combined launch vehicle and satellite system. More specifically relates to the satellite combined with the launch vehicle's upper stage to provide a more efficient system that includes tank separation technology which allows the satellite system to shed tanks that have used up all the propellants stored therein. The method separation of the tank set is enabled by using a merman band or pneumatic type of separation system; wherein the three bottom tanks (105) are emptied first (202) during the process, followed by the separation of the emptied tanks (203) herein the fuel is completely filled in the second set of tanks (203). The first pair of tanks (103) is then separated after the fuel is emptied (204). Similarly, the plumbing lines (106) are also separated along-with. The separation of the used components is achieved herein (205) and the satellite is ready for orbit insertion (206).
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