An apparatus to house a rotorcraft , comprising: a first container ; a first container leg disposed on a first corner of the first container ; a second container leg disposed on a second corner of the first container ; a third container leg disposed on a third corner of the first container ; a fourth container leg disposed on a fourth corner of the first container , at least one of the first, second, third, and fourth container legs having a lower portion with a first ramped foot having a first angled face and a protrusion and an upper portion having a ramped receiving slot with a second angled face and an opening , wherein the first angled face is at a complementary angle with the second angled face , and wherein the opening of the ramped receiving slot is configured to receive a protrusion associated with a second ramped foot of a second container , when stacked above the first container , with the second angled face of the ramped receiving slot of the upper portion of the leg of the first container configured to interface with a first angled face of a lower portion of a leg of the second container , the protrusion thereof placed in and extending through the opening , and wherein the protrusion of the first ramped foot of the lower portion of the at least one of the first, second, third, and fourth container legs has a hole for inserting a retaining pin to ensure that the protrusion is prevented from backing out of an opening of a ramp receiving slot associated with an upper portion of the leg of the second container , when stacked below the first container, such that the stacked containers do not disconnect; a hinged wall cover extending between the first corner and the second corner of the first container , the hinged wall cover having a wall actuator to open and close the hinged wall cover ; and a landing pad , an actuator arm operative to extend and retract the landing pad to retrieve the rotorcraft . a first container ; a first container leg disposed on a first corner of the first container ; a second container leg disposed on a second corner of the first container ; a third container leg disposed on a third corner of the first container ; a fourth container leg disposed on a fourth corner of the first container , at least one of the first, second, third, and fourth container legs having a lower portion with a first ramped foot having a first angled face and a protrusion and an upper portion having a ramped receiving slot with a second angled face and an opening , wherein the first angled face is at a complementary angle with the second angled face , and wherein the opening of the ramped receiving slot is configured to receive a protrusion associated with a second ramped foot of a second container , when stacked above the first container , with the second angled face of the ramped receiving slot of the upper portion of the leg of the first container configured to interface with a first angled face of a lower portion of a leg of the second container , the protrusion thereof placed in and extending through the opening , and wherein the protrusion of the first ramped foot of the lower portion of the at least one of the first, second, third, and fourth container legs has a hole for inserting a retaining pin to ensure that the protrusion is prevented from backing out of an opening of a ramp receiving slot associated with an upper portion of the leg of the second container , when stacked below the first container, such that the stacked containers do not disconnect; a hinged wall cover extending between the first corner and the second corner of the first container , the hinged wall cover having a wall actuator to open and close the hinged wall cover ; and a landing pad , an actuator arm operative to extend and retract the landing pad to retrieve the rotorcraft . <EOS>