CV: Post Grad in Space Engineering and Rocketry



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Candidate Profile
 Date Submitted:09-08-2011
 Last Modified:10-08-2011 (08:20)
Job information
 Current job:Post Grad in Space Engineering and Rocketry
 Employment Term:Permanent
 Job location:Anywhere
 Date available:immediately
 Industry:Launch Systems


To successfully meet the challenges brought by the revolutionary changes in the Space Field.



Sex: Male                                              Marital Status: Single

Date of Birth: 14th January, 1988              Languages Known: English, Telugu, and Hindi



Birla Institute of Technology                              Ranchi- Mesra

M.E, Department of Space Engineering & Rocketry                       2009 – 2011

Specialization: Rocket Propulsion

Overall CGPA: 7.95/10


MLR Institute of Technology (JNTU)                          Hyderabad

Bachelors of Aeronautical Engineering                               2005 – 2009

Overall Percentage: 68.76


Nalanda Educational Institutions                            Vijayawada

Intermediate- Board of Intermediate Education                              2003 – 2005

Overall Percentage: 84


Nagarjuna Public School                          Pedavadlapudi

Secondary School Certificate                            2005

Overall Percentage: 72




M.E Project: Investigation of Thrust – Vector Control Studies using Jet Vanes

Organization: Birla Institute of Technology (BIT-Mesra)


Thrust vector control (TVC) methods were developed as an alternative to aerodynamic control surfaces for missiles, which suffered from poor pitch- over characteristics in launching stage.TVC system, can allow the missile to turn quickly and stably in any direction by deflecting the nozzle exhaust gas irrespective of the missile speed. A jet vane is one of such devices, used for thrust vectoring. An effort has been made to evolve a methodology that can be used to develop a jet vane, that is lighter in weight and / or smaller in size for a given control force. Computations have been performed to analyze the jet vane at high temperatures at different angles of attack.

The aerodynamic performance of a jet vane has also been determined at Mach number 2 in a supersonic wind tunnel at ambient conditions. In another experimental set up the jet vane erosion has been determined by placing a mild steel jet vane in the stream of exhaust gases at different angles of attack.


B.Tech. Project:Analysis of Aerofoil Aerodynamic Characteristics and Design Optimization

Organization: MLR Institute of Technology (MLRIT - Hyderabad)

Shape of the symmetric aerofoil is altered by changing their coordinates forming a personalized aerofoil, tested in virtual wind tunnel for the aerodynamic characteristics such as lift and drag, coefficients of lift and drag, pressure coefficient, moment coefficient  of newly designed modifies aerofoil. There have been eight different profiles shaped from the standard NACA 0012 aerofoil with no changes in the maximum thickness in percent of chord, but with a change in the position of that thickness from the leading edge of the aerofoil along the chord. Among the eight, one profile illustrates the best aerodynamic characteristics when compared to the standard aerofoil chosen for study.

Significant Project Works done during the Academic Batch of 2005-2009:       

Mini Project: Manufacturing on Compressor Assembly in Tecumseh Pvt. Ltd. Balanagar, Hyderabad.  

Mini Project: Hydraulics cylinder in Redsson Industries Pvt. Ltd.

Mini Project: Oscillating Cylinder Mechanism in MLR Institute of Technology

Team member in “The Reconstruction of Pushpak aircraft” MLR Institute of Technology, Hyderabad during September 2007.


CATIA-Full Time Course from CITD, Hyderabad, summer 2006.

MATLAB- One Week Program Organized by Department of Electronics and Communication, College of Engineering, Osmania University, Hyderabad.



Programming Languages: C

Software Packages: AutoCAD, Ansys CFX, Catia V5, Gambit, Fluent, & Solid works.




1.    Elements of Aerodynamics

2.    Elements of Rocket Propulsion

3.     Engineering & Space Flight

4.    Fundamentals of Combustion

5.    Solid Rocket Propulsion

6.    Liquid & Hybrid Rocket Propulsion

7.    Advance Propulsion Systems

8.    Rocket Combustion Process

9.    Propellant Technology



REFERENCE: 1                                               REFERENCE: 2

Dr.A.K.Chatterji                                                  Dr. J. K. Prasad

HOD of Space Engg & Rocketry                         Professor

BIT-Mesra, Ranchi, Jharkhand                             BIT- Mesra, Ranchi, Jharkhand

Mail Id: akchatterjee(at)                   Mail Id: jkprasad(at)


REFERENCE: 3                                              REFERENCE: 4

Dr. Mohan Varma                                               Dr. P. C. Joshi

Professor                                                            Professor

BIT- Mesra, Ranchi, Jharkhand                           BIT- Mesra, Ranchi, Jharkhand

Mail Id: mohanvarma(at)                 Mail Id: pcjoshi(at)



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