Foreign bank: means a foreign bank, as defined in the International Banking Act of 1978 §.Fiduciary: A trustee, executor, or administrator.Fiduciary: means trustee, agent, executor, administrator, committee, guardian or conservator for a minor or other incompetent person, receiver, trustee in bankruptcy, assignee for creditors or any holders of a similar position of trust.Executor: includes an administrator, where the subject matter applies to an administrator.Executor: A male person named in a will to carry out the decedent.Deposit: means a deposit of money, bonds or other things of value, creating a debtor-creditor relationship.Department: means the department of financial institutions.Corporation: A legal entity owned by the holders of shares of stock that have been issued, and that can own, receive, and transfer property, and carry on business in its own name.Company: includes a bank, trust company, corporation, partnership, association, business or other trust, or similar business entity.Community: means a city, town, or incorporated village in this state, or where not within any of the foregoing, a trade area in this state. ![]() Commissioner: means the commissioner of financial institutions.Beneficiary: A person who is entitled to receive the benefits or proceeds of a will, trust, insurance policy, retirement plan, annuity, or other contract.Bankruptcy judges preside over these proceedings. Under the protection of the bankruptcy court, debtors may discharge their debts, perhaps by paying a portion of each debt. Bankruptcy: Refers to statutes and judicial proceedings involving persons or businesses that cannot pay their debts and seek the assistance of the court in getting a fresh start.Bank: means any person, as hereinafter defined, doing a banking business subject to the laws of this or any other jurisdiction and, for the purposes of supervision, examination and liquidation, includes industrial investment companies and industrial banks authorized by chapter 5 of this title.Agent: means any person duly authorized in writing by a lessee to enter a safe deposit box rented by the lessee, whether the person be denominated as "agent" "deputy" "attorney-in-fact" or otherwise.The proposed safety analysis is applied to a fictitious 2U CubeSat mission that performs a controlled re-entry using the Drag De-orbit Device developed by the ADAMUS laboratory at the University of Florida.Terms Used In Tennessee Code > Title 45 > Chapter 2 > Part 9 - Safe Deposit and Safekeeping Coupled with advanced statistical techniques designed to estimate very low probabilities such as the Inputs' Statistics Method, a reliable safety analysis can be conducted with a limited overall computational burden. ![]() The reduced order model is based on these high level variables and captures the spacecraft fragmentation behavior and its re-entry dynamics with significantly less computation time than the high fidelity model. The high fidelity model includes both the aerodynamic and aerothermodynamic effects that occur during re-entry and is used to statistically characterize “high level’’ uncertain variables such as the ballistic coefficient and the demise altitude. This proposed safety analysis is achieved using two re-entry models of differing complexity. Furthermore, by estimating the probability of debris landing outside the largest possible safety box within which there is a zero casualty risk, the maximum probability of control failure admissible for the mission can be estimated. Correctly estimating the dimensions of a safety box and locating it over uninhabited regions, such as the oceans, guarantees a casualty risk below a prescribed value. A simple geometric safety assessment is proposed, based on the safety boxes concept introduced in the ESA Space Debris Mitigation Compliance Verification Guidelines. The objective of this work is to provide a reliable and efficient statistical analysis to estimate the risk to aeronautic and maritime traffic as well as to ground based populations. In addition, these spacecraft are usually limited to shallow re-entries which are more sensitive to atmospheric model uncertainties and thus have larger debris fields. They may contain components which might withstand the re-entry conditions and reach the ground. Indeed, small spacecraft able to achieve advanced mission objectives are more frequently on the worldwide space agenda. While in the past the end-of-life design for this type of spacecraft was often approximated or totally neglected, it has recently become increasingly important. ![]() In recent years, the interest and demand for small satellites have grown exponentially.
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