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The State‐of‐the‐Art Model Atmosphere From the Surface to 110 km Over the Indian Tropical Region for ISRO Launching Vehicle Applications: Developed From In Situ and Space‐Based Measurements

Earth and space science (Hoboken, N.J.), 2023-01, Vol.10 (1), p.n/a

2023

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Concept design and planning of India's first interplanetary mission

Current science (Bangalore), 2015-09, Vol.109 (6), p.1050-1054

Adimurthy, V.

2015

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Computation of Non-Equilibrium Chemically Reacting Hypersonic Flow from a Cartesian Mesh with Near Wall Viscous Resolution

Journal of applied fluid mechanics, 2014-04, Vol.7 (2), p.217-226

2014

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Computation of Heat Flux in Hypersonic Flow with a Cartesian Mesh Using Near-Wall Resolution

Journal of Aerospace Sciences and Technologies, 2023-08, p.166-177

2023

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Correlated Atmospheric Variations Using Optimization of Dft Parameters for Monte Carlo Simulations Of Indian Space Missionscorrelated Atmospheric Variations Using Optimization of Dft Parameters for Monte Carlo Simulations Of Indian Space Missions

Journal of Aerospace Sciences and Technologies, 2023-07, p.207-219

2023

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Parameter Optimization with Chebyshev Polynomials for Trajectory Design of A RLV

Journal of Aerospace Sciences and Technologies, 2023-08, p.31-37

2023

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An empirical model for the tropical Indian region using in-situ and space-borne observations taking into account of tropical oscillations

Advances in space research, 2024-05, Vol.73 (9), p.4621-4633

2024

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Multidisciplinary Optimization Aerospace Design: The Emerging Technology For Complex Systems

Journal of Aerospace Sciences and Technologies, 2023-08, p.79-92

2023

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Nonimpact Lunar Transfer Trajectories Using the Pseudostate Technique

Journal of guidance, control, and dynamics, 2005-03, Vol.28 (2), p.217-225

2005

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Space mission planning and operations

Current science (Bangalore), 2007-12, Vol.93 (12), p.1791-1811

2007

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An analysis of near-circular lunar mapping orbits

Journal of Earth System Science, 2005-12, Vol.114 (6), p.619-626

2005

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Precise Lunar Gravity Assist Transfers to Geostationary Orbits

Journal of guidance, control, and dynamics, 2006-03, Vol.29 (2), p.500-502

2006

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Lifting Re-entry Trajectory Optimization

Journal of Aerospace Sciences and Technologies, 2023-08, p.239-246

2023

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Space debris mitigation measures in India

Acta astronautica, 2006-02, Vol.58 (3), p.168-174

2006

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Consideration of lifetime limitation for spent stages in GTO

Advances in space research, 2004, Vol.34 (5), p.1227-1232

2004

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Launch strategy for Indian lunar mission and precision injection to the Moon using genetic algorithm

Journal of Earth System Science, 2005-12, Vol.114 (6), p.711-716

2005

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Space debris proximity analysis in powered and orbital phases during satellite launch

Advances in space research, 2004, Vol.34 (5), p.1125-1129

2004

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A method of calculating fragment velocity additions for the analysis of the breakup of a launch vehicle upper stage

Advances in space research, 2004, Vol.34 (5), p.1246-1250

2004

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Separation Dynamics of Strap-On Boosters in the Atmosphere

Journal of guidance, control, and dynamics, 1997-07, Vol.20 (4), p.633-639

1997

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Separation dynamics of ullage rockets

Journal of guidance, control, and dynamics, 1994-05, Vol.17 (3), p.426-434

1994

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Separation dynamics of heat shield fairings

Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 1997-01, Vol.211 (2), p.67-80

1997

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Separation dynamics of strap-on boosters

Journal of guidance, control, and dynamics, 1992-01, Vol.15 (1), p.137-143

1992

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Launch vehicle trajectory optimization including rotational dynamics

Journal of spacecraft and rockets, 1976-01, Vol.13 (1), p.59-61

Adimurthy, V

1976

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Spin rate variations of spin-stabilized apogee motors in thrust phase

Journal of guidance, control, and dynamics, 1988-07, Vol.11 (4), p.382-383

1988

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Trajectory and attitude determination of a thrusting spin-stabilizedapogee stage

Journal of guidance, control, and dynamics, 1987-05, Vol.10 (3), p.276-282

1987

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The State‐of‐the‐Art Model Atmosphere From the Surface to 110 km Over the Indian Tropical Region for ISRO Launching Vehicle Applications: Developed From In Situ and Space‐Based Measurements

Concept design and planning of India's first interplanetary mission

Computation of Non-Equilibrium Chemically Reacting Hypersonic Flow from a Cartesian Mesh with Near Wall Viscous Resolution

Computation of Heat Flux in Hypersonic Flow with a Cartesian Mesh Using Near-Wall Resolution

Correlated Atmospheric Variations Using Optimization of Dft Parameters for Monte Carlo Simulations Of Indian Space Missionscorrelated Atmospheric Variations Using Optimization of Dft Parameters for Monte Carlo Simulations Of Indian Space Missions

Parameter Optimization with Chebyshev Polynomials for Trajectory Design of A RLV

An empirical model for the tropical Indian region using in-situ and space-borne observations taking into account of tropical oscillations

Multidisciplinary Optimization Aerospace Design: The Emerging Technology For Complex Systems

Nonimpact Lunar Transfer Trajectories Using the Pseudostate Technique

Space mission planning and operations

An analysis of near-circular lunar mapping orbits

Precise Lunar Gravity Assist Transfers to Geostationary Orbits

Lifting Re-entry Trajectory Optimization

Space debris mitigation measures in India

Consideration of lifetime limitation for spent stages in GTO

Launch strategy for Indian lunar mission and precision injection to the Moon using genetic algorithm

Space debris proximity analysis in powered and orbital phases during satellite launch

A method of calculating fragment velocity additions for the analysis of the breakup of a launch vehicle upper stage

Separation Dynamics of Strap-On Boosters in the Atmosphere

Separation dynamics of ullage rockets

Separation dynamics of heat shield fairings

Separation dynamics of strap-on boosters

Launch vehicle trajectory optimization including rotational dynamics

Spin rate variations of spin-stabilized apogee motors in thrust phase

Trajectory and attitude determination of a thrusting spin-stabilizedapogee stage

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