ALBERT

Description: Abstract 2458 Poster Board II-435 Introduction: When used as therapy for hematopoietic malignances, allogeneic hematopoietic stem cell transplantation (HCT) relies on the graft-versus-leukemia (GVL) effect to eradicate residual tumor cells through immunologic mechanisms. However, graft-versus-host-disease (GVHD) is a potentially lethal complication of allogeneic BMT. Thus, inhibition of GVHD, while preserving GVL and protective responses against infectious agents, can enhance the therapeutic potential of BMT. GVHD is initiated by alloreactive donor T cells that recognize mismatched major and/or minor histocompatibility antigens and cause severe damage to hematopoietic and epithelial tissues. Protein kinase C theta isoform (PKCθ) is crucial in TCR signaling and regulates the nature of lymphocyte-specific effector responses. The aim of this study was to investigate the significance of PKCθ in donor T-cell-mediated GVHD, anti-leukemia, and antiviral infection. Methods: Our results were validated using clinically relevant murine bone marrow transplantation (BMT) models. GVHD was measured by recipient survival and clinical signs such as body weight loss. Leukemia/lymphoma was induced by intravenous injection of a luciferase expressing A20 clone (a B lymphoma cell line derived from BALB/c mice). Tumor invasion was quantitated using the Xenogen IVIS-200 bioluminescence imaging system. Murine cytomegalovirus (MCMV) infection was induced by intraperitoneally injecting MCMV in the recipients after GVHD was established. Results: Using 3 distinct mouse models of allogeneic BMT, we found that T cells lacking PKCθ are unable to undergo robust expansion and cause damage to recipient hematopoietic or epithelial tissues, demonstrating that an essential requirement for PKCθ in alloreactivity and GVHD development. In contrast, PKCθ-/- T cells retain the ability to respond to virus infection post-BMT. Mechanistically, absence of PKCθ raises the threshold for T cell activation that selectively impacts alloresponses, but T cell responses triggered by infection or following administration of antigen plus microbial adjuvant are relatively well preserved in the absence of PKCθ Furthermore, we evaluated the role of PKCθ in GVHD and GVL responses, and found that PKCθ-/- T cells have at least a 10-fold reduction in the ability to induce GVHD but only a ∼2.5-fold reduction in GVL compared to WT T cells. Thus, absence of PKCθ impacts GVHD responses more significantly than GVL responses. Conclusion: These findings validate PKCθ as a potentially unique therapeutic target that is required for GVHD induction but not for GVL or protective responses to infectious agents in allogeneic BMT. Disclosures: No relevant conflicts of interest to declare.

Description: This paper presents the analytical formulation and numerical results for heat transfer in a high heat flux condenser that relies on capillary flow along shaped fins (Gregorig surfaces) and a drainage network embedded in the condenser walls. Results are shown for a variety of fin profile shapes in order to show the geometric trade-offs involved in seeking a maximum effective heat transfer coefficient for the fin. Predictions of the model show excellent agreement with previously reported measurements for steam. Based on this work, a profile has been selected for a 2 kW ammonia condenser currently under development for use in space. In that design the fin half width is 0.5 mm and the model predicts a heat transfer coefficient referred to the base of the fin of 9 W/sq cm deg C for a heat flux of 10/W sq cm at the base.

Description: Future evolution and growth of the Space Station will place increasing demands on the thermal management system by the addition of new payloads and from increased activity in the habitat modules. To meet this need, Creare is developing advanced evaporators, condensors, and single-phase heat exchangers for operation in microgravity. The objective is to achieve a several-fold increase in the heat flux capability of these components, while operating at the same temperature difference as specified for the present interface heat exchangers. Two prototype interface heat exchangers are presently being developed: one to interface the main thermal bus to a payload two-phase ammonia bus, and the other, to interface with the crew module single-phase water loop. The results achieved to date in the development of these heat exchangers are reviewed.

Description: This paper presents the results obtained to date in a program to develop a high heat flux, single-phase heat exchanger for spacecraft thermal management. The intended application is a net generation interface heat exchanger to couple the crew module water thermal bus to the two-phase ammonia main thermal bus in the Space Station Freedom. The large size of the interface heat exchanger is dictated by the relatively poor water-side heat transfer characteristics. The objective of this program is to develop a single-phase heat transfer approach which can achieve heat fluxes and heat transfer coefficients comparable to those of the evaporation ammonia side. A new heat exchanger concept has been developed to meet these objecties. The main feature of this heat exchanger is that it can achieve very high heat fluxes with a pressure drop one to two orders of magnitude lower than those of previous microchannel or jet impingement high heat flux heat exchangers. This paper describes proof-of-concept experiments performed in air and water and presents analytical model of the heat exchanger.

Description: This report describes the development of a high performance, all metal compact heat exchanger. The device is designed for use in a reverse Brayton cryogenic cooler which provides five watts of refrigeration at 70 K. The heat exchanger consists of a stainless steel tube concentrically assembled within a second stainless steel tube. Approximately 300 pairs of slotted copper disks and matching annular slotted copper plates are positioned along the centerline axis of the concentric tubes. Each of the disks and plates has approximately 1200 precise slots machined by means of a special electric discharge process. Positioning of the disk and plate pairs is accomplished by means of dimples in the surface of the tubes. Mechanical and thermal connections between the tubes and plate/disk pairs are made by solder joints. The heat exchanger assembly is 9 cm in diameter by 50 cm in length and has a mass of 10 kg. The predicted thermal effectiveness is greater than 0.985 at design conditions. Pressure loss at design conditions is less than 5 kPa in both fluid passages. Tests were performed on a subassembly of plates integrally soldered to two end headers. The measured thermal effectiveness of the test article exceeded predicted levels. Pressure losses were negligibly higher than predictions.

Description: Proposed heat-exchange scheme boosts heat transfer per unit area. Key component is generator that fires uniform size droplets of subcooled liquid at hot plate. On impact, droplets spread out and evaporate almost instantly, removing heat from plate. In practice, many generator nozzles arrayed over evaporator plate.

Description: Proposed gas-circulating machine consists essentially of centrifugal pump driven by induction motor. Noncontact bearings suppress wear and contamination. Used to circulate helium (or possibly hydrogen or another gas) in regeneration sorption-compressor refrigeration system aboard spacecraft. Also proves useful in terrestrial applications in which long life, reliability, and low contamination essential.