ARC ADEPT — Adaptable Deployable Entry and Placement Technology¶
FO provided the suborbital flight test that validated ADEPT's deployment and aerodynamic performance — a mechanically deployable aeroshell for planetary entry.
Created: Session 97, 2026-04-07
Last updated: Session 97, 2026-04-07
Summary¶
ADEPT is a deployable aeroshell (like a folded umbrella that opens into a heat shield) for planetary entry, descent, and landing. Game Changing Development (GCD) funded the core technology development; Flight Opportunities funded the SR-1 sounding rocket flight test on September 12, 2018, using UP Aerospace's SpaceLoft XL at White Sands. The flight successfully demonstrated exo-atmospheric deployment and stable supersonic-to-subsonic entry. ADEPT remains at concept maturity for Venus, Mars, and Titan missions — no mission has yet selected it.
FO Project¶
91412 — ADEPT Flight Testing¶
| Field | Value |
|---|---|
| Lead Org | Ames Research Center |
| PI | Paul F. Wercinski |
| Period | 2014-08-28 to 2019-10-11 |
| TRL | 4 → 5 |
| Status | Completed |
| TX | TX09.4.5: Integrated Modeling and Simulation for EDL |
SR-1 Flight Test (September 12, 2018): - Vehicle: 0.7m deployed diameter ADEPT on UP Aerospace SpaceLoft XL sounding rocket - Location: White Sands Missile Range, NM - Objectives: (1) Demonstrate stow-separate-deploy sequence in exo-atmospheric zero-g; (2) Characterize aerodynamic performance of faceted blunt-body geometry during supersonic-to-subsonic deceleration - Results: On-board video confirmed deployment achieved and maintained. Post-flight analysis showed stable flight below Mach 0.8. Both primary objectives met.
Connection to UP Aerospace: ADEPT flew on the same SpaceLoft XL platform used for UP Aerospace's own SPYDER missions (94196, 94202, 106636). See UP Aerospace page.
GCD Parent Projects¶
| Project | Period | TRL | Description |
|---|---|---|---|
| 13596 ADEPT | 2014-2016 | 3→6 | Core technology development — fabric TPS, rib/strut mechanisms |
| 94041 ADEPT/SR-1 | 2016-2019 | 3→5 | SR-1 flight experiment preparation and execution (GCD-funded) |
| 116322 ADEPT-Spider weave | 2019-2021 | 3→4 | Post-SR-1 thermal testing of woven TPS (Bally Ribbon Mills) |
FO's role: GCD funded the technology development and experiment preparation; FO funded the suborbital flight test environment. This is a co-funded maturation model where FO provides the flight access.
Mission Concepts Studied¶
ADEPT has been proposed for multiple planetary destinations but has not been selected for any mission:
- Venus: Aerocapture for small satellite missions. Studies suggest 70% payload increase vs. propulsive orbit insertion. Papers: NTRS 20190011701 (2019).
- Mars: SmallSat delivery to Mars surface. "Enabling New and Innovative Low Cost Mars Science" (Low Cost Mars Workshop 2022, Wercinski presentation).
- Titan: Entry system for Titan exploration concepts.
- Earth return: CubeSat and SmallSat Earth return from orbit.
- "Dandelander" concept: ADEPT-based delivery of small surface payloads (referenced in TechPort).
Publications¶
- NTRS 20190028862: "ADEPT Sounding Rocket One Flight Test Overview" (2019)
- NTRS 20190031937: "ADEPT Sounding Rocket One (SR-1) Flight Test" (2019)
- NTRS 20180006874: "ADEPT SR-1 Development and Testing" (2018)
- NTRS 20190002830: "ADEPT, A Mechanically Deployable Re-Entry Vehicle System, Enabling Interplanetary CubeSat and Small Satellite Missions" (SmallSat Conference)
- AGU 2020: "The Adaptable, Deployable, Entry and Placement Technology (ADEPT) enabling advanced entry, descent, and landing capabilities for SmallSat missions"
Outcome Assessment¶
| Category | Assessment |
|---|---|
| Outcome | Technology Ready, Awaiting Mission Selection |
| TRL achieved | 5 (FO) / 6 (GCD overall) |
| Mission infusion | No — no mission has selected ADEPT |
| Commercial | No — NASA center technology |
| Follow-on funding | GCD continued post-SR-1 with Spider weave testing |
| Publications | 5+ NTRS papers + conference presentations |
| Time since FO flight | 7.5 years (Sep 2018 → Apr 2026) |
Assessment: ADEPT is technically successful — the SR-1 flight met both objectives. But without a mission selecting a deployable aeroshell for EDL, the technology remains in the "ready but waiting" state. This is a common pattern for NASA center EDL technologies: high TRL achieved, but mission selection depends on science objectives and decadal survey priorities that are outside the technology developer's control.
Verification¶
| Claim | Evidence | Confidence |
|---|---|---|
| SR-1 flight occurred Sep 12, 2018 | NTRS papers, NASA image gallery | Confirmed |
| SR-1 met both objectives | NTRS 20190028862, on-board video | Confirmed |
| Flew on UP Aerospace SpaceLoft XL | NTRS, NASA descriptions | Confirmed |
| No mission has selected ADEPT | No mission references found in web search | Confirmed (negative) |
| GCD funded overall program; FO funded flight test | TechPort [91412] (FO) + [94041] (GCD) | Confirmed |
Related Pages¶
- UP Aerospace — launch provider for SR-1
- HeetShield — another FO-funded entry technology (HIAD TPS)
- FO Mission Infusion Summary