fig1 illustrates an embodiment of the present invention , the first par being a bolster table 100 including a bolster plate 102 with a ply of material 106 that has been applied across heating elements 103 and held in position by bolster plate pins 101 which are in turn held in place by grooves 104 and hooks and 105 . the heating elements 103 are mounted in grooves 117 of the bolster plate 102 . the top portion of an individual heating element 103 preferably includes an electric strip heater 118 mounted atop a compliant insulating layer , preferably of 90 durometer silicone rubber . the bolster plate is preferably made of steel . the pins 101 of the several embodiments of the present invention are preferably stainless steel rectangular parallelepipeds . other pins providing a rectangular contact surface and able to withstand the heat and pressure required are also acceptable . fig2 illustrates an apparatus 200 having the bolster plate 102 with fabric and bolster plate pins 101 being placed into the press 207 . heating elements 103 in the bolster plate are aligned with a set of fixture pins 208 in a grooved alignment fixture 209 in the press 207 . fig3 illustrates the bolster plate 102 with fabric 106 and bolster plate pins 101 aligned with the fixture pins 208 in the grooved alignment fixture 209 in the press 207 where the heating elements 103 provide heat and concentrate pressure during each nodal cure cycle . fig4 illustrates the node curing of the first ply 106 . the press 107 is adjusted to apply the appropriate amount of pressure at the contact surfaces , or nodes , of the fabric between each fixture pin 208 and each heating element 103 . once each portion of the ply 401 between the fixture pin 208 and heating element 103 ( i . e ., the node 402 ) has been pressed and heated a sufficient time for the node 402 to be cured , the electric strip heater 118 are switched off , and the press 207 is retracted . the bolster plate pins 101 are then removed . many fabrics are applicable to the ply or plies of the several embodiments of the present invention . the prepreg fabric can be one or more plies of uncured unidirectional material and preferably the fabric is kevlar ® or a similar aromatic polyamide fiber of high tensile strength . in addition , the fabric may be a sheet of resin impregnated felt , a sheet of stitched unidirectional fabric , a sheet of chopped - fiber reinforced molding material or a sheet of unreinforced sheet molding compound . fig5 illustrates the newly formed ply 401 being shifted laterally 510 the distance of one - half cell , before being reinserted into the apparatus 200 on top of the fixture pins 208 . the bolster plate 102 is removed and prepared for the next ply . the second ply 501 is aligned into the bolster plate 102 in a manner as done with the initial alignment of the first ply and then the second ply 501 is held in position by the reinserted bolster plate pins 101 . the bolster plate 102 is reinserted into the press 207 . fig6 illustrates the co - curing of the first ply 401 and the second ply 501 . pressure ( e . g ., 40 pounds per square inch ) generated by the press 207 and heat from electric strip heater elements 118 are applied to the top surface and bottom surface of each of the nodes 601 , thereby curing the nodes 601 . fig7 illustrates that once the nodes 601 are cured , the fixture pins 208 at the cured surfaces are removed . the bolster plate pins 101 , enclosed by each of the resulting cells 701 , are kept in place . the entire honeycomb core 702 with bolster plate pins 101 is shifted laterally 705 one - half cell , i . e ., one - half of a corrugation period , and realigned into the grooved fixture 209 of the press 207 . the first set of bolster plate pins 101 now function as a second set of fixture pins 101 for the next iteration of ply application . the bolster plate 102 is removed and the next ply of material 710 is applied to the bolster plate 102 and the next ply of material 710 is held in place by the first set of fixture pins 208 now functioning as a second set of bolster plate pins 208 . the bolster plate 102 is placed into the press 207 where pressure and heat by way of the heating elements 103 and the first set of bolster plate pins 101 , now functioning as a second set of fixture pins 101 , are applied at the nodal surfaces of the core 702 and the next ply of material 710 . the second set of fixture pins 101 are removed and the entire core 702 translated one - half of a corrugation cycle in a core - centering direction 710 with the second set of bolster plate pins 208 enclosed by the resulting cells of the second layer 501 and the third layer 710 and with the second set of bolster plate pins 208 aligned with a respective heating element 103 . the second set of bolster plate pins 208 now function as the first set of fixture pins 208 and the second set of fixture pins 101 now function as bolster plate pins 101 . thereafter , the cycle repeats until a core 702 desired core height is achieved ( fig8 ). once the core has reached the desired height , pins are removed and the core is placed in an oven for final curing . the above process is disclosed in flowchart form in fig9 a , 9 b and 9 c . the flowchart of fig9 a illustrates that the process begins 905 with providing a bolster table 100 including a steel plate 102 having a plurality of transverse rectangular grooves 117 and a plurality of groove - mounted pins 101 , preferably rectangular parallelepipeds , retractably and translationally mounted coplanar with the bolster plate 102 and providing an apparatus for receiving the bolster table 100 including a press 207 and a fixture 209 comprising a plurality of pins 208 that are preferably rectangular parallelepipeds 910 . the process continues 915 with drawing a sheet of prepregnated fabric 106 across the bolster plate 102 having heating elements . then the flowchart of fig9 b illustrates that the process continues with the inserting the bolster plate 102 into the receiving press 207 so that the top surfaces of the heating elements 103 and the bottom surfaces of the fixture pins 208 are substantially aligned 920 . next , the bolster plate 102 is pressed so that the heating elements 103 press portions of the fabric of at least one ply 106 against the fixture pins 925 . next 930 , portions of the fabric of at least one ply 106 are heated by the heating elements 103 . then 935 , if this is the first ply , the press 207 is retracted , the bolster plate 102 removed , the fabric 106 is removed and translated by one - half of a corrugation period and reinserted into the bolster table 100 so as to rest upon the tops of the bolster plate pins 101 , optionally removing the heating elements 103 , and cleaning the bolster plate as needed 940 . if this is not the first ply 935 , then the flowchart of fig9 c illustrates that the press 207 is retracted 942 , the bolster plate pins 101 are removed , the fixture pins 208 are translated one - half of a corrugation period and with them the plies of the article thus formed 702 . next 945 the bolster plate 102 is pressed such that the hating elements 103 press portions of the article 702 against the first set of bolster plate pins 101 , now functioning as a second set of fixture pins , and heating those portions of the article by way of the heating elements 103 . next , the press 207 is retracted , the bolster plate 102 and the fixture pins 208 , now functioning as a second set of bolster pins 208 , are removed , and the bolster plate pins 101 , i . e ., the second set of fixture pins 101 , are translated by one - half of a corrugation period in a restoring direction , and a third ply is inserted into the bolster table 100 so as to rest upon the tops of the fixture pins 208 , i . e ., the second set of bolster plate pins 208 , and thereafter the heating elements are optionally removed and the bolster plate is cleaned as needed 950 . the process iterates 952 until a desired core size 720 is achieved . thereafter , the article 720 is removed from the apparatus and post - cured 955 . the words used in this specification to describe the invention and its various embodiments are to be understood not only in the sense of their commonly defined meanings , but to include by special definition in this specification structure , material or acts beyond the scope of the commonly defined meanings . thus if an element can be understood in the context of this specification as including more than one meaning , then its use in a claim must be understood as being generic to all possible meanings supported by the specification and by the word itself . the definitions of the words or elements of the following claims are , therefore , defined in this specification to include not only the combination of elements which are literally set forth , but all equivalent structure , material or acts for performing substantially the same function in substantially the same way to obtain substantially the same result . in addition to the equivalents of the claimed elements , obvious substitutions now or later known to one with ordinary skill in the art are defined to be within the scope of the defined elements . the claims are thus to be understood to include what is specifically illustrated and described above , what is conceptually equivalent , what can be obviously substituted and also what essentially incorporates the essential idea of the invention .