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Dinesh Kumar, B.
- Preclinical Bioavailability-Bioequivalence and Toxico-Kinetic Profile of Stable Succinc Acid Cocrystal of Temozolomide
Abstract Views :307 |
PDF Views:123
Authors
Edula Sravani
1,
M. K. Chaitanya Mannava
2,
Damandeep Kaur
3,
B. R. Annapurna
1,
Ronaq Ali Khan
3,
Kuthuru Suresh
3,
Sudhir Mittapalli
3,
Ashwini Nangia
2,
B. Dinesh Kumar
1
Affiliations
1 Centre for Advanced Research for Pre-Clinical Toxicology, Food and Drug Toxicology Research Centre, National Institute of Nutrition (Indian Council of Medical Research), Hyderabad 500 007, IN
2 Crystalin Research Private Limited, Technology Business Incubator, University of Hyderabad Campus, Hyderabad 500 046, IN
3 School of Chemistry, University of Hyderabad, Central University P.O., Prof. C. R. Rao Road, Hyderabad 500 046, IN
1 Centre for Advanced Research for Pre-Clinical Toxicology, Food and Drug Toxicology Research Centre, National Institute of Nutrition (Indian Council of Medical Research), Hyderabad 500 007, IN
2 Crystalin Research Private Limited, Technology Business Incubator, University of Hyderabad Campus, Hyderabad 500 046, IN
3 School of Chemistry, University of Hyderabad, Central University P.O., Prof. C. R. Rao Road, Hyderabad 500 046, IN
Source
Current Science, Vol 108, No 6 (2015), Pagination: 1097-1106Abstract
Temozolomide (TMZ) is a frontline prodrug for the treatment of glioblastoma multiforme (brain cancer) approved by the US-FDA in 1999. A limitation with this otherwise potent and selective DNA alkylating agent is degradation of the prodrug to the inactive product 5-aminoimidazole-4-carboxamide (AIC) by incipient hydrolysis during storage. This transformation not only makes the drug less effective (due to hydrolysis of the active drug), but also causes discoloration from white to pink and tan brown colour (due to AIC contamination), which can make patients anxious and suspicious about the drug efficacy. We solved the stability issue of TMZ by preparing its succinic acid (SA) cocrystal and showed that TMZ-SA is stable for over 6 months in accelerated stability conditions of 40°C, 75% RH, as confirmed by PXRD. TMZ-SA retained its white colour for over 6 months compared to the tan-brown discoloration for TMZ in less than 1 month. Based on the enhanced stability and comparable dissolution profile of TMZ-SA, we now take forward TMZ-SA pharmaceutical cocrystal to stability assessment by HPLC analysis and preclinical bioavailability and bioequivalence with the reference drug. We observed that there were no significant differences in the pharmacokinetic profile of the test cocrystal TMZ-SA compared to standard drug TMZ in Sprague Dawley rats. The bioavailability ratio was found to be in the range 102-109%. Pharmacokinetic parameters such as Tmax, Cmax, T1/2, AUC and Ke are slightly superior for TMZ-SA and the toxico-kinetic profile is also better than TMZ. Most significantly, it has been shown that the active drug is released from the hydrogen-bonded cocrystal and was detected in the brain tissue of rats. Thus we report on a pharmaceutical cocrystal complying with the United States Food and Drug Administration guidance on pharmaceutical cocrystals. These results suggest that TMZSA cocrystal with improved physico-chemical properties is bioequivalent and has superior stability compared to the reference drug TMZ and a potential lead for an improved TMZ formulation.Keywords
Bioavailability, Bioequivalence, Cocrystal, Glioma, Toxico-Kinetic Profile.- Vectoring Tests on Flex Nozzle System of Solid Rocket Motor Using Electro Mechanical Actuators
Abstract Views :501 |
PDF Views:4
Authors
Affiliations
1 Advanced Systems Laboratory, Kanchanbagh, Hyderabad, IN
1 Advanced Systems Laboratory, Kanchanbagh, Hyderabad, IN
Source
Manufacturing Technology Today, Vol 16, No 1 (2017), Pagination: 3-8Abstract
Vectoring tests are carried out on each flex nozzle system of a rocket motor to verify the performance of flex seal using Electro Mechanical actuators, mirror image sensors and electronic controller. These tests are done for acceptance of the flex nozzle control system in the missile. The flex nozzle controls are tested for sine, ramp, frequency, response commands. During the tests the Command, Pitch, Average, Main Voltages are recorded using DAC. The flex nozzle system is integrated to the pressure chamber in horizontal condition and the Electro Mechanical actuators and mirror image sensors are assembled to the flex nozzle systems. The Electro Mechanical actuators are connected to the battery or 70V power supply to operate the actuators. Then the vectoring tests are performed using the Electro Mechanical actuators. LVDT'S are mounted on nozzle for displacement measurement. The chamber is pressurized pneumatically up to 2 bar.Keywords
Flex Nozzle System, Electro Mechanical Actuators, Vectoring Tests, Digital Controllers.References
- Sutton, George P: Rocket Propulsion Elements, Inter science Publication John Wiley & Sons Inc, 8th Edition January 2010.
- Ray, SK: Missile Control Systems, DESIDOC Publications, New Delhi, 2007.
- Ram Mohan CH. V; Ramanathan, J; Satish Kumar; Gupta, AVSSKS: Characterization of materials used in Flex bearing of Large Solid Rocket Motors, 'Defence science Journal', vol. 61, no. 3 May 2011, 264-269.
- Scott C, Asbury; Jeffrey A, Yetter: Static Performance of Six Innovative Thrust Reverser Concepts for Subsonic Transport Applications, DIANE Publishing, 1-2, ISBN- 978-1-4289-9643-4, 10th July 2013.
- Megysey Eugene F: Pressure Vessel Hand book, PV publishing INC. Oklahoma City, USA, 14th edition.
- Kadam, NV: Practical Design of Flex Control System for Launch Electro Mechanical Vehicle & Missiles, Allied Publishers Pvt. Ltd, Jan 2006.
- Maclsaue, Bernie; Langton, Roy: Gas Turbine Propulsion System, John Wiley & Sons, 152-155, ISBN 978-0-470-0653-1.
- Kuphaldt, Tony R: Lesson in Electrical circuits, vol. 4, Chapter-6 Ladder Logic, September 2010.
- Brady, Ian: Programmable Logic Controllers Benefits & applications PLCS”, 5th December, 2011.
- Balakrishna, R: Guided Weapons System Design, DESIDOC Publications, New Delhi, 1998 ◘
- Design and Analysis of Crankshaft Used in Aerospace Applications and Comparision Using Different Materials
Abstract Views :135 |
PDF Views:0
Authors
Affiliations
1 Aerospace Engineering, MLR Institute of Technology, Hyderabad, IN
1 Aerospace Engineering, MLR Institute of Technology, Hyderabad, IN