Patent Awaiting formal examination

DESIGN AND MANUFACTURING OF A SINGLE PIECE ROCKET ENGINE

LaoBiz.com profiles the Laos Patent “DESIGN AND MANUFACTURING OF A SINGLE PIECE ROCKET ENGINE” from open registry fields, filed by AGNIKUL COSMOS PRIVATE LIMITED on 2010-10-23; current status: Awaiting formal examination. Identifiers include application No. P/895; DIP id LAP895; protection kind Patent - PCT National Phase. Key dates: publication 2026-04-03. Classification: B33Y 50/00. Inventor(s)/designer(s): RAVICHANDRAN, Srinath, SHAH KHADRI, Syed Peer Mohamed. Abstract hint: Disclosed herein is a single piece, integrated, light weighted, cost-effective 3D printed engine for space vehicles. FIG. 5 illustrates an…. Status labels may change after office actions; refresh or consult primary DIP data before commercial decisions.

Patent Laos DIP

App. no. P/895
Filing date 2010-10-23
Applicant AGNIKUL COSMOS PRIVATE LIMITED
Agent ACTIP (LAO) IP CO., LTD.
Classes B33Y 50/00

Mark

Key facts

Type
Patent
App. no.
P/895
Status
Awaiting formal examination
Applicant
AGNIKUL COSMOS PRIVATE LIMITED
Agent
ACTIP (LAO) IP CO., LTD.
Filing date
2010-10-23
Publication
2026-04-03
Protection kind
Patent - PCT National Phase
Priority
IN · 202041046382 · 2020-10-23
Nice / IPC classes
B33Y 50/00
Goods / services

Process

Steps follow the current public status
  1. Filed
  2. Formal examination In progress
  3. Substantive examination
  4. Published
  5. Granted

Related records

Linked from the LaoBiz.com company database

Abstract

Disclosed herein is a single piece, integrated, light weighted, cost-effective 3D printed engine for space vehicles. FIG. 5 illustrates an integrated engine that comprises a combustion chamber to burn the fuel, an injector plate (504) to inject the fuel to the combustion chamber, an igniter (502) to ignite the fuel mixture, anozzle (506) to pass hot gas to produce thrust and cooling channels (508) for regenerative cooling, where all these components are fused to form a single piece integrated engine. The engine of the present invention eliminates the need of assembling the individual components. Further, the engine is additively manufactured with high grade aerospace materials. Thus, the cost and mass of the engine is reduced when compared to traditionally manufactured engines, which leads to frequent missions.

Disclosed herein is a single piece, integrated, light weighted, cost-effective 3D printed engine for space vehicles. FIG. 5 illustrates an integrated engine that comprises a combustion chamber to burn the fuel, an injector plate (504) to inject the fuel to the combustion chamber, an igniter (502) to ignite the fuel mixture, anozzle (506) to pass hot gas to produce thrust and cooling channels (508) for regenerative cooling, where all these components are fused to form a single piece integrated engine. The engine of the present invention eliminates the need of assembling the individual components. Further, the engine is additively manufactured with high grade aerospace materials. Thus, the cost and mass of the engine is reduced when compared to traditionally manufactured engines, which leads to frequent missions.

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