Operating sequence / orbital delivery

From cassette to orbit.

Follow one CubeSat through storage, guided feed, custody handoff and commanded release. Then inspect the host-assisted orbit change and a matched spring-deployer comparison.

3 minutes 10 seconds

One complete explanation.

Still view of the VOLLEY inventory at the beginning of the operating cycle.

Reduced motion is enabled. Read the transcript or still sequence below, or choose playback.

HD 1280 × 720 · 24 fps · English on-screen explanation and optional captions · silent film · playback by choice

Choose a chapter

Mechanism, comparison and mission.

00:00 · The mechanism

Actual Blender motion of accepted CAD parts: pallet retrieval, one-cell feed, loaded lift, positive handoff, launch, arrest and return.

Watch the 70-second chapter →

01:10 · Deployment principles

A spring-canister schematic and a powered-carrier schematic. Product details vary; prior adjustable mechanisms are acknowledged.

Watch the 20-second comparison →

01:30 · Orbital delivery

A generic maneuverable upper stage makes the coarse change. The commanded release sets a local relative velocity. Same-state spring and ideal preset comparisons follow.

Watch the 100-second chapter →
Still alternative

Read the sequence without motion.

Twelve inspected stages from storage through guided feed, transfer, release and return.
CAD-derived Blender sequence. Other cells and mounting parts are hidden in detail views; nominal spring reference envelopes are omitted. Timing is edited for explanation.
Five orbital chapters showing coarse host transfer, relative release, matched spring comparison and distinct speed scenarios.
Invariant-checked planar two-body illustrations with explicit physical scales and magnified relative views. The stage is a generic surrogate.
Interpret the speeds

Separate configurations and evidence.

CaseRole in the film
1, 2 and 3 m/s commandsCurrent ACR1 computational command points. The source-coupled 3 m/s example includes finite host/sled recoil.
0.2 m/sIllustrative inertial kick outside the current evaluated command points.
About 16 m/sHistorical periodic-model speed used as a kinematic example; not a current ACR1 rating.
1 km/s and beyondSeparate future kinematic research cases. They do not depict present rail capability.

The coarse example uses an ideal same-plane 500 → 600 km Hohmann transfer: 27.42 m/s, coast, then 27.32 m/s circularization. The current release example enters an ellipse; reaching a higher circular orbit requires another propulsion event. The ideal preset spring matches the same ideal trajectory. No new navigation-accuracy or system-superiority claim follows from this film.

Editable sources

Inspect and reproduce the explanation.

The source package contains the baked Blender scene, generators, trajectory data, inputs, captions and verification records. The original accepted source identities remain pinned; display motion is distinct from contact dynamics.