WEBVTT 00:00:00.000 --> 00:00:04.000 Retain the inventory Twelve 3U envelopes. Two independent six-cell banks. 00:00:04.000 --> 00:00:10.000 Retrieve the captive pallet The lift grips the reusable pallet before carrier locks release. 00:00:10.000 --> 00:00:16.000 Index to the selected cell The pallet rises to the source-cell loading plane. 00:00:16.000 --> 00:00:25.000 Feed one CubeSat Storage keepers open. Guided lead-screw pusher advances 250 mm. 00:00:25.000 --> 00:00:30.000 Secure the transfer Lift keepers retain the payload. Pusher retracts; cell gates close. 00:00:30.000 --> 00:00:38.000 Lower to the launch plane Loaded lift moves from 830 mm to the 46 mm launch datum. 00:00:38.000 --> 00:00:43.000 Transfer custody to the sled Carrier locks engage before the lift releases its pallet grips. 00:00:43.000 --> 00:00:49.000 Clear. Prove. Arm. Lift clear. Pallet locked. Source and arrest path ready. 00:00:49.000 --> 00:00:54.000 Accelerate the loaded sled 1.300 m powered stroke. Evaluated commands: 1, 2 and 3 m/s. 00:00:54.000 --> 00:00:58.000 Release the CubeSat The payload departs; the pallet remains attached to the sled. 00:00:58.000 --> 00:01:05.000 Arrest and return the carrier 210 mm arrest allocation. Retained carrier and pallet return. 00:01:05.000 --> 00:01:10.000 Index the next retained cell Eleven payloads remain. Repeat the controlled sequence. 00:01:10.000 --> 00:01:20.000 Passive canisters release stored spring energy; VOLLEY commands a powered stroke. Both start from the host-established orbital state. 00:01:20.000 --> 00:01:30.000 Host trims or an ideal preset spring can match preplanned targets. Actual deployer mechanisms and separation settings vary. 00:01:30.000 --> 00:01:35.000 A generic restart-capable upper stage supplies the coarse move from 500 km circular. 00:01:35.000 --> 00:01:40.000 A +27.42 m/s tangential burn enters the transfer ellipse. 00:01:40.000 --> 00:01:45.000 Coast for 47.82 minutes in the same orbital plane. 00:01:45.000 --> 00:01:50.000 A second +27.32 m/s burn circularizes the host at 600 km. 00:01:50.000 --> 00:01:55.000 At delivery, VOLLEY sets the relative release vector; the host supplies maneuver authority. 00:01:55.000 --> 00:02:00.000 Current ACR1 computations evaluate command points 1, 2 and 3 m/s. 00:02:00.000 --> 00:02:05.000 The 3 m/s command gives a modeled payload inertial kick of 2.92694 m/s. 00:02:05.000 --> 00:02:10.000 Retained sled motion and host recoil are included. The local schematic is not to scale. 00:02:10.000 --> 00:02:15.000 Compare the same 600 km host state with a representative 1 m/s passive spring. 00:02:15.000 --> 00:02:20.000 The 1 m/s P-POD-style example is a comparison choice, not a universal product rating. 00:02:20.000 --> 00:02:25.000 An ideal ground-preset spring can match the same kick and the same ideal trajectory. 00:02:25.000 --> 00:02:30.000 The 24-hour co-rotating zoom has separately scaled axes. It is not navigation accuracy. 00:02:30.000 --> 00:02:35.000 The 3 m/s command example creates a 600 by 610.82 km ellipse. 00:02:35.000 --> 00:02:40.000 Perigee remains at 600 km. The orbital period is about 96.80 minutes. 00:02:40.000 --> 00:02:45.000 A circle at apogee requires another propulsion event: about +2.926 m/s here. 00:02:45.000 --> 00:02:50.000 Coast follows the ellipse. Circularization requires a separate burn. 00:02:50.000 --> 00:02:54.000 0.2 m/s is an illustration outside the current evaluated command points. 00:02:54.000 --> 00:02:58.000 Current modeled points are 1, 2 and 3 m/s. This view shows the 3 m/s command. 00:02:58.000 --> 00:03:02.000 About 16 m/s is a historical periodic-model result, not a current ACR1 rating. 00:03:02.000 --> 00:03:06.000 1 km/s is future kinematic research, shown separately from the current rail. 00:03:06.000 --> 00:03:10.000 3.5 km/s gives an unbound path: a future kinematic case, not current rail capability.