Abstract: Techniques for deploying a plurality of smallsats from a common launch vehicle are disclosed where a structural arrangement provides a load path between an upper stage of the launch and the plurality of spacecraft. Each spacecraft is mechanically coupled with the launch vehicle upper stage only by the structural arrangement. The structural arrangement includes at least one trunk member that is approximately aligned with the longitudinal axis of the launch vehicle upper stage, a plurality of branch members, each branch member being attached to the trunk member and having at least a first end portion that is substantially outboard from the longitudinal axis; and a plurality of mechanical linkages, each linkage coupled at a first end with a first respective spacecraft and coupled at a second end with one of the plurality of branch members, the trunk member or a second respective spacecraft.

Abstract: A spacecraft with a linear extension boom, an antenna feed, and a rigid antenna reflector is provided. The rigid antenna reflector may be connected with one end of the linear extension boom, and the other end of the linear extension boom may be connected with the spacecraft main body. In a launch configuration of the spacecraft, the linear extension boom may be retracted into a stowed configuration, and in an on-orbit configuration of the spacecraft, the linear extension boom may be extended into a deployed configuration, thereby moving the rigid antenna reflector away from the yaw axis of the spacecraft and positioning the rigid antenna reflector such that the focal point of the rigid antenna reflector may be oriented to align on, and be collocated with, the antenna feed. The rigid antenna reflector may be connected with the linear extension boom by a positioning mechanism that provides for adjustment in the angular orientation of the rigid antenna reflector relative to the linear extension boom.

Abstract: A launch vehicle includes an upper stage and an integral fairing. In a launch configuration, the integral fairing is configured to enclose, between an aft portion and a forward portion, one or more payloads. The integral fairing includes a mechanical attachment with the upper stage proximal to the aft portion, and a nose cap proximal to the forward portion and a passive venting arrangement that equalizes pressures internal and external to the integral fairing. The integral fairing is configured to permit deployment of at least one payload, while avoiding: (i) separation of the integral fairing into two or more parts, (ii) separation of the integral fairing from the upper stage, and (iii) articulation of the mechanical attachment. The upper stage may provide single stage to orbit capability.

Abstract: A spacecraft includes an aft surface, a forward surface and a main body structure disposed therebetween, a stowage and deployment arrangement (SDA) joined to the main body structure by a first mechanical coupling, and an antenna that includes a respective feed element and a rigid antenna reflector coupled with the main body by way of the SDA. The feed element is joined to the main body structure by a second, different, mechanical coupling. The spacecraft is reconfigurable from a launch configuration, with the reflector is disposed forward of the forward surface, with its aperture plane substantially parallel to the forward surface, to an on-orbit configuration. The SDA repositions the reflector to a second position corresponding to the on-orbit configuration. In the second position, the reflector is disposed, Earth facing, substantially aft of the forward surface and outboard of the main body structure and is illuminated by the respective feed element.

Abstract: A spacecraft with a linear extension boom, an antenna feed, and a rigid antenna reflector is provided. The rigid antenna reflector may be connected with one end of the linear extension boom, and the other end of the linear extension boom may be connected with the spacecraft main body. In a launch configuration of the spacecraft, the linear extension boom may be retracted into a stowed configuration, and in an on-orbit configuration of the spacecraft, the linear extension boom may be extended into a deployed configuration, thereby moving the rigid antenna reflector away from the yaw axis of the spacecraft and positioning the rigid antenna reflector such that the focal point of the rigid antenna reflector may be oriented to align on, and be collocated with, the antenna feed. The rigid antenna reflector may be connected with the linear extension boom by a positioning mechanism that provides for adjustment in the angular orientation of the rigid antenna reflector relative to the linear extension boom.

Abstract: A method for monitoring the status of documents created by a large scale document production and management process. The production and management process may be comprised of a plurality of different stages including: utilizing a print stream to generate the documents, printing documents on a printer in accordance with the print stream, and forming completed mail pieces on an inserter from the printed documents in accordance with mail piece creation data files. A monitoring system receives information regarding the status of individual documents within these production and management process stages. A user may then select one of the stages for closer inspection of the status of documents. For the selected stage, status of individual documents is displayed.

Abstract: A system for providing real-time, integrated production of individually addressed sealed envelopes containing personalized printed material matched to individual addresses, the system including at least one printing controller capable of receiving personalized printing data from at least one data source, the personalized printing data including envelope address information for a multiplicity of envelopes and personalized envelope contents information which varies for the multiplicity of envelopes and is matched to individual envelope addresses, the at least one printing controller being operative to merge and order the personalized printing data from the at least one data source such that it is printed in a desired distribution sorting order, selected to optimize postal savings in bulk mailings and at least one production facility for the individually addressed sealed envelopes containing personalized printed material matched to individual addresses, each of the at least one production facility including at l

Abstract: A system, method and apparatus for preparing mailpieces. A inserter system for assembling mailpieces in a mailing job is controlled in accordance with mailpiece records in a corresponding mailing control file. The inserter system scans control inserts included in the mailpieces fed into the mailpiece accumulations at a downstream station to verify corresponding mailpiece records. Initially the inserter system reads an initial, dummy control insert to accesses the mailing control file to initialized the upstream stations of the inserter system.

Abstract: A system, method and apparatus for preparing mailpieces. A inserter system for assembling mailpieces in a mailing job is controlled in accordance with mailpiece records in a corresponding mailing control file. The inserter system scans control inserts included in the mailpieces fed into the mailpiece accumulations at a downstream station to verify corresponding mailpiece records. Initially the inserter system reads an initial, dummy control insert to accesses the mailing control file to initialized the upstream stations of the inserter system.

Abstract: A system for gathering and transmitting detailed inserter machine data to one or more clients. The inserter controller gathers substantially all significant machine data from machine sensors and control routines data relating to the operation of the machine and the processing of mail pieces. The gathered data is stored in a compressed format in journal format. A data pump processes the compressed journal data, extracting those parts that are of interest, and transmitting them to client applications in a format that is easily interpreted. The data pump processing includes selecting a subset of data from the journal that is of interest to the particular client.

Abstract: A system, method and apparatus for preparing mailpieces. A inserter system for assembling mailpieces in a mailing job is controlled in accordance with mailpiece records in a corresponding mailing control file. The inserter system scans control inserts included in the mailpieces fed into the mailpiece accumulations at a downstream station to verify corresponding mailpiece records. Initially the inserter system reads an initial, dummy control insert to accesses the mailing control file to initialized the upstream stations of the inserter system.

Abstract: A system, method and apparatus for preparing mailpieces. A inserter system for assembling mailpieces in a mailing job is controlled in accordance with mailpiece records in a corresponding mailing control file. The inserter system scans control documents included in the mailpieces to identify corresponding mailpiece records. Initially the inserter system accesses the mailing control file to identify set-up parameter values for the current mailing job.

Abstract: An apparatus for assembling mailpieces and a method for controlling such apparatus. The apparatus includes a document feeder for feeding sets of documents to a chassis for assembly into mailpieces a constant rate. Because the number of documents varies the time to assemble a set varies and it is possible that a set may not be available when the chassis is ready to cycle; resulting in a cycle in which no mailpiece is processed. To correct for this the average number of documents for a number of mailpieces to be processed is determined and a nominal chassis speed and cycling rate are determined correspondingly. The actual chassis speed is then periodically updated to approach the nominal speed.

Abstract: A method and system for preparing mailpieces. A inserter system for assembling mailpieces in a mailing job is controlled in accordance with a measure of the fraction of chassis cycles which are empty. The chassis speed is continually adjusted during run-time for a mailing job to minimize the number of “dry holes”, i.e. the fraction of chassis cycles which do not contain a mailpiece.

Abstract: A method for controlling an inserter system having a chassis for assembling mailpieces, the chassis operating cyclically with successive accumulations advancing at the end of each cycle. The inserter system further includes a document feeder for feeding accumulations of documents to the chassis, the accumulations containing varying numbers of documents whereby the document feeder is operated at a first speed such that accumulations are available for input to the chassis at varying intervals substantially depending upon the number of documents in corresponding accumulations. And the chassis is operated at a selected speed, which speed is periodically updated in dependence upon the number of documents in the corresponding accumulations in the document feeder.

Abstract: A method and system for tracking manually repaired mailpieces and the like. Control documents are produced by a data processing system and transported to an inserter system. The inserter system inputs the control documents and assembles mailpieces in accordance with mailpiece records identified by coded information on the documents. If a damaged mailpiece is manually repaired an operator scans the coded information from the damaged mailpiece. A data processing system accesses the mailpiece record in accordance with the scanned information and updates the corresponding mailpiece record to reflect manual repair of the document.

Abstract: A mail sender processes batches of mail each of which is accompanied by a statement summarizing the type and number of mail pieces sent and amount of postage for each batch. During processing, each mail piece is identified by a unique number for security purposes.

Abstract: An inserter based mail manifesting system includes a controller that processes sensed information and generates a manifest that can accompany mail to a postal depository.

Abstract: The present invention is directed to a system wherein a mailer is able to send large quantities or batches of mail. The mailer has a secure accounting unit similar to a postage meter in which postage value is placed by a central station which is also in communication with a remote resetting center for accounting for funds transferred to the accounting unit. The central station communicates with the mailing station in order to obtain data relative to the mail processing whenever the funds are to be transferred to the accounting unit. The central station may also serve to lock or unlock the mail processing at the mailing station. Receipts may also be provided for the funding transactions.

Abstract: Apparatus is provided for transporting a sheet in a predetermined path of travel. The apparatus comprises a plate having a lower surface extending parallel to and defining the path of travel, and having an aperture formed therein. In addition, the apparatus comprises sheet feeding structure, including a first pair of rollers spaced apart from one another and an endless belt looped about the first rollers, wherein the belt has a lower belt run extending between the first rollers and beneath the plate. Further, the feeding structure includes instrumentalities for driving one of the first rollers for moving the lower belt run at a constant velocity in the direction of the path of travel. Moreover, the feeding structure includes a second pair of rollers which are disposed beneath the plate and are made of a compliant material.