Publications

THESIS

PhD in Energy and Environment
Next generation low/zero emission hypersonic vehicles.

MSc in Satellite Engineering

Design and Sizing of a Hybrid Rocket Engine for Air Launch Applications.

Special Master of Aerospace Engineering

Experimental Investigation of the Paraffin Thermomechanical Properties and Hybrid Rocket Engine Performance for Different Fuel Grain Formulations.

Advisor: Prof. Antonella Ingenito, Prof. Patrick Hendrick, Prof. Stefano Vecchio Ciprioti

ARTICLES

Review on the regression rate-improvement techniques and mechanical performance of hybrid rocket fuels

Y Pal, SN Mahottamananda, SK Palateerdham, S Subha, A Ingenito

FirePhysChem 1 (4), 272-282

Hybrid Machine Learning Approach for Gully Erosion Mapping Susceptibility at a Watershed Scale (I.F - 3.1)

Sliman Hitouri, Antonietta Varasano, Meriame M, Safae Ijlil, N Essahlaoui, Sk Ajim Ali, A Essahlaoui, Q B Pham, Mirza Waleed,S K Palateerdham, Ana Cláudia Teodoro

ISPRS International Journal of Geo-Information 2022, 11(7), 401; https://doi.org/10.3390/ijgi11070401

Thermal decomposition kinetics and combustion performance of paraffin-based fuel in the presence of CeO2 catalyst

Yash Pal, Sri Nithya Mahottamananda, S Subha, Sasi Kiran Palateerdham, Antonella Ingenito

FirePhysChem - Elsevier

Combustion performance of hybrid rocket fuels loaded with MgB2 and carbon black additives (I.F - 4.563 )

YashPal, Sasi Kiran Palateerdham, Sri NithyaMahottamananda, SubhaSivakumar, Antonella Ingenito

Propulsion and Power Research

Array of carbon black-based microthrusters for CubeSat applications - FirePhysChem, 2024, 4(2), pp. 87–94

Antonella Ingenito, Sasi Kiran Palateerdham, M. Panzanaro

Oxidation reaction kinetics of HTPB-boron carbide/polytetrafluoroethylene formulations as a solid fuel (I.F - 8.035)

Yash Pal, Sri Nithya Mahottamananda, Sasi Kiran Palateerdham, Antonella Ingenito, Djalal Trache

Theoretical Understanding of the Effects of High-density Energetic Particles on the Ramjet Performance

Sasi Kiran Palateerdham, Abdul Rahman, Antonella Ingenito, Sri Nithya Mahottamananda, Yash Pal

Journal of Propulsion and Energy - The Korean Society of Propulsion Engineers.

CONFERENCE PROCEEDINGS

Understanding the total pressure losses nature in a Scramjet Combustor (AIAA 2023-3040)

Sasi Kiran Palateerdham, Lakshmi Narayana Phaneendra Peri, Antonella Ingenito, Yash Pal, and Sri Nithya Mahottamananda

25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, May 28 - June 1, 2023, India

Design and experimental set-up of a paraffin-based hybrid rocket engine to brake a 24U microsatellite in a Mars orbit

Caio Henrique F.L.D, Sasi Kiran Palateerdham, Antonella Ingenito, Stefano Vecchio

5th IAA Conference on University Missions and CubeSat Workshop, Rome

SHAR for a TSTO Launcher

Naresh Relangi, L.N. Phaneendra Peri, Sasi Kiran Palateerdham, and Antonella Ingenito

25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, May 28 - June 1, 2023, India

Numerical investigation of the impact of injectors' location on fuel mixing in the HIFiRE 2 Scramjet combustor

Sasi Kiran Palateerdham*, Lakshmi Narayana Phaneendra Peri, Antonella Ingenito, Ashish Vashishtha

EUCASS 2023

3D Printed Miniaturized Micro Thrusters for CubeSat Applications

Sasi Kiran Palateerdham*, KR Perumal, A Ingenito, R Andriani, M Panzanaro, LN Phaneendra Peri;

74th International Astronautical Congress 2023

Numerical Study of Hydrogen Injection to Initiate Oblique Detonation Wave

Ashish Vashishtha, Rushikesh Kore, Sasi Kiran Palateerdham, Antonella Ingenito