Abstract: Pointing interfaces that can be used to assemble/disassemble instruments/payloads from a spacecraft/host are disclosed. The disclosed interfaces provide structural, communications, power, and fluid connections (for thermal control). Such interfaces also provide active and passive vibration isolation capability for precision pointing. They can further act as an interface to the launch vehicle for secondary delivery of the instrument/payload to the spacecraft.

Abstract: Pointing interfaces that can be used to assemble/disassemble instruments/payloads from a spacecraft/host are disclosed. The disclosed interfaces provide structural, communications, power, and fluid connections (for thermal control). Such interfaces also provide active and passive vibration isolation capability for precision pointing.

Abstract: One embodiment of the invention provides a perfusion system including: a first circuit adapted and configured to circulate a first perfusate through a lumen of a small intestine and a second circuit adapted and configured to circulate a second perfusate through one or more blood vessels of the small intestine. Another aspect of the invention provides a method of perfusing at least a portion of a small intestine. The method includes: circulating a first perfusate through a lumen of the small intestine and circulating a second perfusate through a blood vessel of the small intestine.