(12) PATENT APPLICATION PUBLICATION (21) Application No.202111046965 A (19) INDIA (22) Date of filing of Application :14/10/2021 (43) Publication Date : 29/10/2021 (54) Title of the invention : A PROCESS OF IMPLEMENTATION OF MUON-CATALYZED FUSION REACTION FOR PROPULSIVE POWER GENERATION IN SPACECRAFTS (71)Name of Applicant : :B64G0001400000, G21B0003000000, (51) International 1)Lovely Professional University B64G0001420000, G21B0001150000, classification Address of Applicant :Jalandhar-Delhi G.T. Road, Phagwara F03H0001000000 144411, Punjab, India ----------- ----------- (86) International :NA Name of Applicant : NA Application No :NA Address of Applicant : NA Filing Date (72)Name of Inventor : (87) International Publication No : NA 1)Kushalin Kashyap 1)Gopalchetty Brahma Address Address of of Applicant Applicant :Lovely :Lovely Professional Professional University, University, Jalandhar- Jalandhar- (61) Patent of Addition :NA Delhi Delhi G.T. Road, Phagwara 144411, Punjab, India G.T. Road, Phagwara 144411, Punjab, India ----------- ----------- ------ ------ to Application Number :NA ----- _____ Filing Date 2)Amit Kumar Thakur (62) Divisional to 2)Gaurav Mehta :NA Address of Applicant :Lovely Professional University, Jalandhar- Application Number Address of Road, Applicant :Lovely Professional :NA Delhi G.T. Phagwara 144411, Punjab,University, Jalandhar- India ----------- ------ Filing Date Delhi G.T. Road, Phagwara 144411, Punjab, India ----------- ------ ----- (57) Abstract : The present invention relates to a method of implementation of muon-catalyzed fusion reaction for propulsive power generation in spacecrafts. In the present disclosure, the muon-catalysed nuclear propulsion process which consists of muon-generator, reaction chamber (7), and an accelerator (9). Here, the entire unit of muon-catalysed nuclear propulsion is to be housed within the spacecraft. The output power is well maintained and properly channelized via confinement through electric and magnetic fields at the accelerator (9) as well as at the inlet to propel the spacecrafts with high power, and increase the velocity of spacecrafts thousand folds as compared to conventional spacecrafts. No. of Pages : 10 No. of Claims : 6 The Patent Office Journal No. 44/2021 Dated 29/10/2021 49947 FORM 5 THE PATENTS ACT, 1970 (39 OF 1970) & THE PATENT RULES, 2003 DECLARATION AS TO INVENTORSHIP [See Section 10(6) and Rule 13 (6)] Lovely Professional University 1. Name of Applicant hereby declare that the true and first inventor(s) of the invention disclosed in the Complete specification filed in pursuance of our application numbered dated …/10/2021 are: 2. Inventor(s) a. Name: KASHYAP, BRAHMA,KUSHALIN Gopalchetty b. Nationality: Indian c. Address: Lovely Professional University, Jalandhar-Delhi G.T. Road, Phagwara 144411, Punjab, India a. Name: MEHTA, THAKUR, GAURAV Amit Kumar b. Nationality: Indian c. Address: Lovely Professional University, Jalandhar-Delhi G.T. Road, Phagwara 144411, Punjab, India 3. Declaration to be given when the application in India is filed by the applicant(s) in the convention country:- We the applicants in the convention country hereby declare that our right to apply for a patent in India is by way of assignment from the true and first inventor(s). 4. Statement (to be signed by the additional inventor(s) not mentioned in the application form) I/We assent to the invention referred to in the above declaration, being included in the complete specification filed in pursuance of the stated application. Dated this …… day of …… 2007. Signature of the additional inventor(s): Name: Dated this….Day of Oct, 2021 Signature Dr. Dharam Buddhi Authorized Signatory Mobile No: 7508182862 To The Controller of Patent, The Patent Office, at Delhi
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