1–20 von 25 Ergebnissen
|

    Utilization of Mechanically Activated Aluminum in Hybrid Rockets

    Marothiya, Gaurav / Ramakrishna, P. A. | AIAA | 2018

    Attaining Hypersonic Flight with Aluminum-Based Fuel-Rich Propellant

    Rathi, Nikunj / Ramakrishna, P. A. | AIAA | 2017

    Enhancement of Hybrid Fuel Regression Rate Using a Bluff Body

    Kumar, Rajiv / Ramakrishna, P. A. | AIAA | 2014

    Enhancing the Regression Rate of Hydroxyl-Terminated-Polybutadiene-Based Mixed Hybrid Rockets

    Marothiya, Gaurav / Kumar, Rajiv / Ramakrishna, P. A. | AIAA | 2022

    Performance Enhancement of a Small Two-Stroke Engine Using Nitromethane Blends

    Raviteja, S. / Ramakrishna, P. A. / Ramesh, A. | AIAA | 2019

    Effects on Burn Rates of Pellets and Propellants with Catalyst-Embedded AP

    Marothiya, Gaurav / Vijay, Chaitanya / Ishitha, K. et al. | AIAA | 2017

    Effect of Accelerated Cyclic Aging on the Ballistic Properties of Composite Solid Propellant

    Yadav, Karri Veerandra / Naseem, Hamza / Murthy, H. et al. | AIAA | 2024

    Attaining Hypersonic Flight with Aluminum-Based Fuel-Rich Propellant

    Rathi, Nikunj | Online Contents | 2017
    Beteiligte: Ramakrishna, P. A

    Burning Rate Studies: Potassium-Doped Ammonium Perchlorate with Other Burn-Rate Modifiers

    Ishitha, Kumar | Online Contents | 2016
    Beteiligte: Ramakrishna, P. A