Abstract: Presented are passive-release, snap-fit coupling devices for attaching cargo to cargo suspension systems, methods for making/using such devices, and aircraft equipped with underbody suspension systems using passive-release, snap-fit coupling devices for securing payloads. An object mounting device is presented for securing an object, such as a cargo container, to a tether hook of a suspension system, such as an aircraft's payload suspension system. The object mounting device includes a base plate that affixes to the object, and a hook latch mounted onto the base plate. The hook latch includes a guide surface adjacent a catch cavity. The catch cavity releasably receives therein the tether hook. The guide surface is oriented at an oblique angle with respect to the base plate in order to slidably engage the tether hook, upon release from the catch cavity and under the force of gravity, to thereby eject the tether hook from the hook latch.

Abstract: Presented are passive-release, snap-fit coupling devices for attaching cargo to cargo suspension systems, methods for making/using such devices, and aircraft equipped with underbody suspension systems using passive-release, snap-fit coupling devices for securing payloads. An object mounting device is presented for securing an object, such as a cargo container, to a tether hook of a suspension system, such as an aircraft's payload suspension system. The object mounting device includes a base plate that affixes to the object, and a hook latch mounted onto the base plate. The hook latch includes a guide surface adjacent a catch cavity. The catch cavity releasably receives therein the tether hook. The guide surface is oriented at an oblique angle with respect to the base plate in order to slidably engage the tether hook, upon release from the catch cavity and under the force of gravity, to thereby eject the tether hook from the hook latch.

Abstract: Disclosed herein is a shaft seal system comprising a first ball bearing, a second ball bearing, a primary shaft seal, and a secondary shaft seal. The secondary shaft seal may be inboard with respect to said primary shaft seal. The shaft seal system can define a leak chamber of a first diameter between said primary shaft seal and a secondary shaft seal. A plurality of O-rings may be further provided between an outer surface of said shaft seal system and said shaft system.

Abstract: Disclosed herein is a cyclonic system for performing subtractive machining in microgravity systems. The cyclonic system comprises: an enclosure, a blower, and a debris collection module to collect the debris from the milling machine. The enclosure includes a top plate, a base plate, and a tapered side wall joining the top plate to the base plate. The enclosure defines a chamber to house a milling machine having a cutter tool. The blower generates an airstream that induces a cyclonic airflow to achieve cyclonic separation of debris within the enclosure. In operation, the cyclonic airflow urges the debris from the milling machine toward the base plate and into the milling machine.

Abstract: Disclosed herein is a shaft seal system comprising a first ball bearing, a second ball bearing, a primary shaft seal, and a secondary shaft seal. The secondary shaft seal may be inboard with respect to said primary shaft seal. The shaft seal system can define a leak chamber of a first diameter between said primary shaft seal and a secondary shaft seal. A plurality of O-rings may be further provided between an outer surface of said shaft seal system and said shaft system.