Three-variant suborbital cargo pod designed for electromagnetic rail launch.
Ballistic delivery of humanitarian and logistics payloads at hypersonic exit velocity. ⚠ v0.1 trajectory claims under forensic review — see Sheet 02 for RK4 simulation results.
DWG MNP-001 | REV 0.1Sheet 01 — Pod Variant Specifications
Variant
Total Mass
Body Diam.
Body Length
CD₀
BC m/(CD·A)
vlaunch @30° elev.
v0.1 Apogee (vacuum)
Manna-B
80 kg [EST]
0.40 m [EST]
1.60 m [EST]
0.40 [EST]
1,592 kg/m² [DERIVED]
4,319 m/s [DERIVED]
247 km ⚠
Manna-I
250 kg [EST]
0.65 m [EST]
2.60 m [EST]
0.42 [EST]
1,794 kg/m² [DERIVED]
7,670 m/s [DERIVED]
850 km ⚠
Manna-H
800 kg [EST]
1.00 m [EST]
4.00 m [EST]
0.45 [EST]
2,264 kg/m² [DERIVED]
10,823 m/s [DERIVED]
1,950 km ⚠
DATA STATUS: All mass, diameter, length, and CD₀ values are preliminary [ESTIMATE] — awaiting structural design, wind-tunnel data, and CFD analysis.
BC and vlaunch are [DERIVED] from vis-viva energy conservation: vz² = 2g₀REh / (RE+h), θ=30°.
v0.1 apogee figures are vacuum claims [PLACEHOLDER] — superseded by atmospheric simulation on Sheet 02.
FINDING (RK4 + US Std Atm 1976):
v0.1 design memo used vacuum constant-g parabolic formula — no atmosphere modeled.
Sea-level dynamic pressure at hypersonic exit velocities (4,319–10,823 m/s) exceeds 11–72 MPa,
producing aerodynamic deceleration of 732–3,231 g.
All three variants are stopped in the lower troposphere (< 10 km AGL).
v0.1 apogee estimates are overestimated by 59–215×.
Architecture redesign required: evacuated launch tube, high-altitude rail site, or significantly reduced exit velocity.
MANNA
Drawing
MNP-002
Title
Trajectory Analysis
Scale
Auto (see canvas)
Model
3-DOF RK4 · dt=0.1 s
Atmosphere
US Std Atm 1976
Date
2026-04-25
Sheet
02 of 02
MANNA EM CARGO PODS · 3 variants · H / I / B · 80–800 kg payloadMANNA-H 100g RATED · bulk cargo · construction · radiation shielding panelsMANNA-I 5.5g RATED · instruments · electronics · scientific payloadsMANNA-B 2.5g RATED · biologics · seeds · medicine · FC-770 shock isolationTRAJECTORY v0.1 SUPERSEDED · RK4 atm sim: 4–9 km apogee (not 247–1,950 km vacuum)BGKPJR RAIL 12 km · 20g · 1,200–1,700 m/s ΔV · VacuumGate IP · patent filedARTEMIS II MISSION COMPLETE · splashdown April 10 2026 · 406,771 km distance recordMISSION EARTH → MOON · rail launch → Space Tug → Blue Moon Mk2 → South Pole colonyBUILT BY Shane Brazelton + Claude Anthropic · Hazel Green, AL · claude.ai/referral/4fAMYN9IngMANNA EM CARGO PODS · 3 variants · H / I / B · 80–800 kg payloadMANNA-H 100g RATED · bulk cargo · construction · radiation shielding panelsMANNA-I 5.5g RATED · instruments · electronics · scientific payloadsMANNA-B 2.5g RATED · biologics · seeds · medicine · FC-770 shock isolationTRAJECTORY v0.1 SUPERSEDED · RK4 atm sim: 4–9 km apogee (not 247–1,950 km vacuum)BGKPJR RAIL 12 km · 20g · 1,200–1,700 m/s ΔV · VacuumGate IP · patent filedARTEMIS II MISSION COMPLETE · splashdown April 10 2026 · 406,771 km distance recordMISSION EARTH → MOON · rail launch → Space Tug → Blue Moon Mk2 → South Pole colonyBUILT BY Shane Brazelton + Claude Anthropic · Hazel Green, AL · claude.ai/referral/4fAMYN9Ing